Fig. 1 Collapse of Shuangyuan Bridge (2009/8/10) (photo courtesy of Apple Daily)

동일한 형상비를 가진 다양한 배치의 교량 교각 주변 세굴에 관한 실험적 연구

동일한 형상비를 가진 다양한 배치의 교량 교각 주변 세굴에 관한 실험적 연구

Experimental study of scour around bridge piers of different arrangements with same aspect ratio

본 연구는 교량 설계 시 중요한 요소인 교각 주변의 국부 세굴 현상을 실험적으로 분석한 보고서입니다. 동일한 형상비(L/B=5)를 유지하면서 교각의 배치를 달리했을 때, 말굽 소용돌이(horse-shoe vortex)와 후류 소용돌이(wake vortex)의 상호작용이 세굴 체적 및 깊이에 미치는 영향을 정량적으로 조사하여 산업적 설계 지침을 제공합니다.

Paper Metadata

  • Industry: 토목 공학 (Civil Engineering)
  • Material: 충적 석영사 (Alluvial quartz sand, d50 = 0.8 mm)
  • Process: 수로 실험 및 세굴 분석 (Flume experiment and scour analysis)

Keywords

  • 교량 교각 (Bridge piers)
  • 국부 세굴 (Local scour)
  • 말굽 소용돌이 (Horse-shoe vortex)
  • 형상비 (Aspect ratio)
  • 실험 수로 (Laboratory flume)
  • 장방형 교각 (Oblong pier)

Executive Summary

Research Architecture

본 연구는 인도 공과대학교(IIT) 봄베이의 수리학 실험실에서 수행되었습니다. 실험 장치는 길이 7.5m, 폭 0.3m, 깊이 0.6m의 재순환식 수로로 구성되었습니다. 실험 대상은 형상비(L/B)가 5로 동일한 세 가지 배치입니다: (a) 직경 0.03m의 원형 교각 2개를 0.15m 간격으로 배치, (b) 동일 직경의 원형 교각 3개를 배치, (c) 폭 0.03m, 길이 0.15m의 단일 장방형(oblong) 교각 배치. 유속 측정에는 3D 음향 도플러 유속계(ADV)인 ‘Vectrino’가 사용되었으며, 세굴 깊이는 포인트 게이지를 통해 측정되었습니다.

Key Findings

실험 결과, 단일 장방형 교각 배치에서 세굴 체적이 가장 적게 나타났습니다. 2개 원형 교각 배치 시 세굴 체적은 3.11×10⁻³ m³였으나, 3개 원형 교각 배치 시 2.44×10⁻³ m³로 21.5% 감소하였고, 단일 장방형 교각의 경우 1.38×10⁻³ m³로 2개 배치 대비 55.63%, 3개 배치 대비 43.44% 감소하였습니다. 이는 단일 구조물이 소용돌이의 강도를 약화시키고 흐름의 분리를 억제하기 때문으로 분석되었습니다. 또한, 상류 교각에서 발생한 후류 소용돌이가 하류 교각의 말굽 소용돌이 형성을 방해하여 하류 측 세굴 깊이가 상대적으로 얕게 나타나는 상호 간섭 현상이 확인되었습니다.

Industrial Applications

본 연구 결과는 교량 기초 설계 시 교각의 형상 및 배치 선정에 직접적인 근거를 제공합니다. 동일한 지지 면적을 확보해야 하는 경우, 여러 개의 원형 교각을 배치하는 것보다 단일 장방형 교각을 사용하는 것이 세굴 위험을 줄이는 데 효과적입니다. 이는 세굴 방지 공사 비용을 절감하고 교량의 구조적 안정성을 높이는 데 기여할 수 있습니다. 또한, 복합 교각 배치 시 발생하는 복잡한 유동장을 이해함으로써 보다 정밀한 수치 모델링 및 설계가 가능해집니다.


Theoretical Background

말굽 소용돌이 (Horse-shoe Vortex) 형성 메커니즘

흐르는 물속에 교각과 같은 장애물이 설치되면 상류 측에 역압력 구배가 발생합니다. 이로 인해 교각 전면에서 하향류(down flow)가 형성되고, 바닥면의 경계층이 분리되면서 말굽 모양의 소용돌이가 생성됩니다. 이 소용돌이는 바닥 전단 응력을 급격히 증가시켜 퇴적물을 비산시키고 교각 주변에 세굴 구멍을 만드는 핵심적인 동역학적 원인으로 작용합니다.

Fig. 1 Collapse of Shuangyuan Bridge (2009/8/10) (photo courtesy of Apple Daily)
Fig. 1 Collapse of Shuangyuan Bridge (2009/8/10) (photo courtesy of Apple Daily)

후류 소용돌이 (Wake Vortex)와 세굴의 관계

교각의 측면에서 분리된 흐름은 교각 배후에서 후류 소용돌이를 형성합니다. 이 소용돌이는 말굽 소용돌이에 의해 부유된 퇴적물을 들어 올려 세굴 구멍 외부로 운반하는 역할을 합니다. 여러 개의 교각이 배치된 경우, 상류 교각에서 발생한 후류 소용돌이는 하류 교각 전면의 유동 구조와 상호작용하여 전체적인 세굴 패턴을 복잡하게 변화시킵니다.

Results and Analysis

Experimental Setup

실험은 0.0003의 일정한 경사를 가진 평면 수로에서 진행되었습니다. 바닥 재료로는 중간 입경(d50) 0.8mm, 비중 2.66인 석영사가 사용되었습니다. 수심은 모래 바닥 위로 16.5cm를 유지하였으며, 유량은 모래의 이동이 시작되는 임계 전단 응력 이하인 0.018 m³/s(최대 유량 기준)로 설정하여 맑은 물 세굴(clear-water scour) 조건을 형성하였습니다. 각 실험은 평형 상태에 도달할 때까지 약 8시간 동안 지속되었습니다.

Visual Data Summary

세굴 등고선(scour contour) 분석 결과, 원형 교각 배치에서는 각 교각 주변에서 개별적인 세굴 구멍이 형성된 후 서로 연결되는 양상을 보였습니다. 반면, 장방형 교각은 상류 선단에서 최대 세굴 깊이가 나타나고 하류로 갈수록 세굴 깊이가 점진적으로 감소하는 안정적인 패턴을 보였습니다. 3개 원형 교각 배치 시 중간 교각은 상류 교각의 후류와 자신의 말굽 소용돌이가 결합되어 복잡한 세굴 형태를 나타냈습니다.

Variable Correlation Analysis

교각의 배치 방식과 세굴 체적 사이에는 뚜렷한 상관관계가 관찰되었습니다. 교각 사이의 간격이 좁을수록(간격/직경 비가 작을수록) 세굴 패턴 간의 간섭이 심화되었습니다. 특히 단일 구조물(장방형)로 통합될 경우, 유동 분리 지점이 줄어들고 소용돌이 시스템의 에너지가 분산되지 않아 세굴 억제 효과가 극대화되었습니다. 이는 구조물의 연속성이 유체역학적 저항을 줄이는 데 결정적인 변수임을 시사합니다.


Paper Details

Experimental study of scour around bridge piers of different arrangements with same aspect ratio

1. Overview

  • Title: Experimental study of scour around bridge piers of different arrangements with same aspect ratio
  • Author: B.A. Vijayasree, T.I. Eldho
  • Year: 2016 (추정, 참조 문헌 기준)
  • Journal: Proceedings of the International Conference on Scour and Erosion (ICSE)

2. Abstract

교량 교각 주변의 세굴은 교량 엔지니어들이 직면한 도전적인 문제입니다. 세굴은 흐름을 방해하는 교각으로 인해 형성된 말굽 소용돌이에 의해 발생합니다. 말굽 소용돌이의 거동은 교각의 배치에 따라 달라집니다. 교각 그룹과 단일 교각의 흐름 패턴은 서로 다르며, 이에 따라 서로 다른 세굴 패턴이 생성됩니다. 본 논문에서는 동일한 형상비를 가진 다양한 배치의 교량 교각 주변 세굴을 실험 수로에서 조사하였습니다. 연구된 세 가지 배치 모두 5의 형상비(L/B)를 가집니다. 실험 수로는 길이 7.5m, 폭 0.3m, 깊이 0.6m이며 재순환 시설을 갖추고 있습니다. 얻어진 결과에 따르면, 단일 고체 교각 주변의 세굴 체적은 교각 조합에 비해 상당히 감소하는 것으로 나타났습니다. 또한, 교각의 조합으로 인해 유동장이 복잡해집니다.

3. Methodology

3.1. 실험 장치 구성: 7.5m 길이의 Plexiglas 수로를 설치하고, 바닥에 0.8mm 입경의 석영사를 채워 실험 환경을 조성함.
3.2. 교각 모델 설치: 형상비 5를 유지하며 원형 교각 2개(배치 a), 3개(배치 b), 장방형 교각 1개(배치 c)를 수로 중앙에 설치함.
3.3. 유동 조건 설정: 0.012, 0.015, 0.018 m³/s의 세 가지 유량을 적용하고, ADV를 사용하여 3차원 유속 데이터를 수집함.
3.4. 세굴 측정: 각 실험을 8시간 동안 수행하여 평형 상태에 도달하게 한 후, 수로의 물을 빼고 포인트 게이지로 세굴 프로파일을 정밀 측정함.

4. Key Results

실험 결과, 단일 장방형 교각(배치 c)의 최대 세굴 깊이는 0.047m로, 원형 교각 배치(0.065m)에 비해 약 28% 감소하였습니다. 세굴 체적 측면에서는 장방형 교각이 1.38×10⁻³ m³를 기록하여, 2개 원형 교각 배치(3.11×10⁻³ m³) 대비 55.63%의 현저한 감소 효과를 보였습니다. 3개 원형 교각 배치의 경우, 중간 교각의 존재가 유동 복잡성을 증가시켰으나 전체 세굴 체적은 2개 배치보다 적은 2.44×10⁻³ m³로 측정되었습니다. 이는 교각 간의 간섭이 소용돌이 강도를 일부 상쇄하기 때문입니다.

5. Mathematical Models

본 연구에서 유동 특성을 정의하기 위해 사용된 주요 무차원 수는 다음과 같습니다.


레이놀즈 수(Reynolds number): $$Re = \frac{uy}{\nu}$$


프루드 수(Froude number): $$Fr = \frac{u}{\sqrt{gy}}$$


여기서 $u$는 유속, $y$는 수심, $\nu$는 물의 동점성 계수, $g$는 중력 가속도를 의미합니다. 실험 시 $Re$는 39370에서 59055 사이, $Fr$은 0.24에서 0.28 사이로 유지되었습니다.

Fig. 9 Two established classifiers for the pile head displacement
Fig. 9 Two established classifiers for the pile head displacement

Figure List

  1. 교각에서의 말굽 소용돌이 및 후류 형성 모식도
  2. 본 연구에 사용된 세 가지 교각 배치 (a, b, c)
  3. 실험 수로의 개략도
  4. 바닥 재료의 입도 분포 곡선
  5. 2개 원형 교각 배치의 시간에 따른 세굴 변화
  6. 2개 원형 교각 배치의 종방향 세굴 패턴
  7. 3개 원형 교각 배치의 시간에 따른 세굴 변화
  8. 3개 원형 교각 배치의 종방향 세굴 패턴
  9. 장방형 교각의 시간에 따른 세굴 변화
  10. 장방형 교각의 종방향 세굴 패턴
  11. 세굴 구멍의 실제 사진 비교
  12. 세 가지 배치에 대한 세굴 등고선도
  13. 세 위치(상류, 중앙, 하류)에서의 횡방향 세굴 프로파일
  14. 세 가지 배치별 세굴 체적 비교 차트

References

  1. Beg, M. (2010). Characteristics of developing scour holes around two piers placed in transverse arrangement.
  2. Beg, M. & Beg, S. (2015). Scour hole characteristics of two unequal size bridge piers in tandem arrangement.
  3. Das, S. and Mazumder, A. (2015). Turbulence flow field around tow eccentric circular piers in scour hole.
  4. Kothyari, U., Garde, R., & Ranga Raju, K. (1992). Temporal Variation of Scour around Circular Bridge Piers.
  5. Melville, B.W. & Chiew, Y.M. (1999). Time scale for local scour at bridge piers.

Technical Q&A

Q: 교각 배치에 따라 세굴 체적이 차이 나는 근본적인 이유는 무엇입니까?

A: 교각이 분리되어 배치될 경우 각 교각에서 독립적인 말굽 소용돌이와 후류 소용돌이가 발생하며, 이들이 상호작용하여 유동 복잡성을 높이고 더 넓은 면적의 바닥 재료를 침식시킵니다. 반면, 단일 장방형 교각은 유동을 더 매끄럽게 유도하고 소용돌이 시스템의 에너지를 집중시켜 분산된 침식을 억제하기 때문에 전체적인 세굴 체적이 감소합니다.

Q: 3개 원형 교각 배치에서 세 번째 교각의 세굴이 음수 값으로 시작하는 이유는 무엇입니까?

A: 실험 초기 단계에서 상류의 첫 번째 및 두 번째 교각 주변에서 침식된 모래 입자들이 하류로 이동하다가 세 번째 교각 전면에 일시적으로 퇴적되기 때문입니다. 흐름이 지속됨에 따라 이 퇴적물들도 결국 세굴되어 사라지며, 약 15분 이후부터 본격적인 세굴 패턴을 따르게 됩니다.

Q: 장방형 교각이 원형 교각 조합보다 세굴 방지에 유리한 정량적 근거는 무엇입니까?

A: 본 실험에서 장방형 교각은 2개 원형 교각 배치 대비 세굴 체적을 55.63% 감소시켰습니다. 또한 최대 세굴 깊이 역시 원형 교각의 0.065m에서 장방형의 0.047m로 약 28% 감소하여, 구조적 안정성 확보에 훨씬 유리함을 입증하였습니다.

Q: 실험에서 사용된 ‘맑은 물 세굴(clear-water scour)’ 조건의 의미는 무엇입니까?

A: 접근 흐름의 전단 응력이 바닥 모래의 이동 임계 전단 응력보다 낮은 상태($u/u_{cr} < 1$)를 의미합니다. 이 조건에서는 일반적인 하천 바닥의 이동은 없으며, 오직 교각 주변에서 강화된 소용돌이에 의해서만 국부적인 세굴이 발생하게 됩니다.

Q: 교각 사이의 간격이 세굴에 미치는 영향에 대한 기존 이론은 무엇입니까?

A: Beg and Beg (2015)의 연구에 따르면, 교각 사이의 순 간격과 교각 직경의 비가 10보다 작을 경우 두 교각의 세굴 패턴 사이에 상호 간섭이 발생합니다. 본 실험에서는 이 비가 1로 매우 작아 강한 간섭 효과가 나타났으며, 이로 인해 하류 교각의 세굴 깊이가 상류보다 낮아지는 현상이 관찰되었습니다.

Conclusion

본 연구를 통해 동일한 형상비를 가진 교각이라도 배치 방식에 따라 세굴 특성이 현저히 달라짐을 확인하였습니다. 단일 장방형 교각은 여러 개의 원형 교각 배치에 비해 세굴 체적과 깊이를 모두 효과적으로 감소시키는 것으로 나타났습니다. 이는 단일 구조물이 말굽 소용돌이의 강도를 약화시키고 유동 구조를 단순화하기 때문입니다. 따라서 경제성과 시공성을 고려하더라도, 세굴 보호 비용과 구조적 안전성을 종합적으로 판단할 때 단일 장방형 교각 설계가 더욱 우수한 대안이 될 수 있음을 시사합니다.


Source Information

Citation: B.A. Vijayasree, T.I. Eldho (2016). Experimental study of scour around bridge piers of different arrangements with same aspect ratio. Proceedings of the International Conference on Scour and Erosion (ICSE).

DOI/Link:

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Figure 2.1: Description of flow structures around a pier (Hodi, 2009)

교량 세굴 예측 최적화: 교각 형상과 희생파일이 안전과 비용을 좌우하는 방법

이 기술 요약은 Mohamed Kharbeche가 2022년 University of Windsor에서 발표한 석사 학위 논문 “The Role of Pier Shape and Aspect Ratio on Local Scour with and Without Sacrificial Piles”를 기반으로 하며, 기술 전문가를 위해 STI C&D가 분석하고 요약했습니다.

키워드

  • Primary Keyword: 교량 세굴
  • Secondary Keywords: CFD, 국소 세굴, 교각 형상, 종횡비, 희생파일, 세굴 방지책

Executive Summary

  • 도전 과제: 기존의 교량 세굴 깊이 예측 모델은 실제보다 과도하게 예측하는 경향이 있어, 비경제적인 교각 설계와 불필요한 비용을 초래합니다.
  • 연구 방법: 실험실 수로에서 다양한 형상(원형, 사각형, 유선형 등)과 종횡비(L/a = 1, 2, 4)를 가진 교각 모델을 사용하여 국소 세굴을 측정하고, 희생파일(sacrificial piles)의 효과를 비교 분석했습니다.
  • 핵심 돌파구: 교각의 형상과 종횡비가 세굴 깊이에 결정적인 영향을 미치며, 뾰족한 유선형(sharp-nosed) 교각과 높은 종횡비가 세굴을 최소화하는 것으로 나타났습니다. 또한 3개의 희생파일 배열이 5개 배열보다 더 효과적인 세굴 감소를 보였습니다.
  • 핵심 결론: 교각의 형상과 종횡비를 최적화하고, 효율적인 세굴 방지책을 적용함으로써 교량의 안전성을 높이고 건설 비용을 절감할 수 있습니다.

도전 과제: 이 연구가 CFD 전문가에게 중요한 이유

교량 붕괴의 약 60%는 교각 주변의 국소 세굴(local scour)과 관련이 있을 정도로, 세굴은 교량의 구조적 안정성을 위협하는 가장 큰 요인 중 하나입니다. 강물의 흐름이 교각과 상호작용하며 기초 주변의 토사를 침식시켜 지지력을 약화시키기 때문입니다.

문제는 현재 북미 표준으로 사용되는 HEC-18과 같은 경험적 세굴 예측 공식들이 종종 세굴 깊이를 과도하게 예측한다는 점입니다. 이는 교각 기초를 불필요하게 깊게 설계하게 만들어 막대한 추가 비용을 발생시킵니다. 이러한 공식들은 교각의 형상(pier shape)이나 길이 대 폭 비율인 종횡비(aspect ratio)와 같은 중요한 변수들의 영향을 충분히 고려하지 못합니다. 따라서 더 정확하고 경제적인 설계를 위해서는 이러한 변수들이 세굴 메커니즘에 미치는 영향을 정밀하게 이해하고, 희생파일과 같은 세굴 방지책의 효율성을 최적화하는 연구가 시급합니다.

연구 접근법: 방법론 분석

본 연구는 캐나다 윈저 대학교(University of Windsor)의 실험 수로(flume)에서 정밀하게 통제된 조건 하에 수행되었습니다.

  • 실험 장비: 길이 10.5m, 폭 1.22m의 수평 실험 수로를 사용하여 실제 하천과 유사한 흐름 환경을 조성했습니다.
  • 핵심 변수:
    • 교각 형상: 원형(Circular), 다이아몬드형(Diamond), 모서리가 둥근 사각형(Round edges), 사각형(Square), 둥근 유선형(Round nose), 뾰족한 유선형(Sharp nose) 등 다양한 형상을 테스트했습니다.
    • 교각 종횡비 (L/a): 교각의 길이(L) 대 폭(a)의 비율을 1, 2, 4로 변경하며 실험을 진행했습니다. 모든 교각의 폭(a)은 51mm로 동일하게 유지했습니다.
    • 세굴 방지책: 교각 상류에 3개 또는 5개의 희생파일(sacrificial piles)을 삼각형 형태로 배열하여 세굴 감소 효과를 비교했습니다.
  • 흐름 조건: 모든 실험은 퇴적물 이동이 막 시작되는 임계유속 직전(U/Uc = 0.9)의 맑은 물 세굴(clear-water scour) 조건에서 수행되었습니다. 유속은 0.28 m/s, 수심은 0.12m로 일정하게 유지했습니다.
  • 데이터 측정: 세굴이 평형 상태에 가까워지는 24시간 동안 실험을 진행한 후, 레이저 거리 측정기(LDM)를 사용하여 세굴 구멍의 중심선과 등고선 프로파일을 정밀하게 측정했습니다. 또한, 레이저 도플러 유속계(LDV)와 음향 도플러 유속계(ADV)를 사용하여 교각 주변의 유속 분포와 난류 특성을 측정했습니다.

핵심 돌파구: 주요 발견 및 데이터

발견 1: 교각 형상과 종횡비가 세굴 깊이를 극적으로 변화시킴

교각의 형상과 종횡비는 세굴 깊이를 결정하는 가장 중요한 요소임이 입증되었습니다.

  • 형상의 영향: 뾰족한 유선형(sharp-nosed) 교각이 모든 종횡비에서 가장 낮은 세굴 깊이를 보였습니다. 반면, 직각 모서리를 가진 사각형 교각(L/a=1)은 원형 교각보다 66% 더 깊은 최대 세굴 깊이(dse/a = 1.75)를 기록했습니다(표 4.2 참조). 이는 흐름의 박리(flow separation)를 최소화하는 유선형 설계가 말굽 와류(horseshoe vortex)의 강도를 약화시켜 세굴을 억제함을 의미합니다.
  • 종횡비의 영향: 동일한 형상에서는 종횡비(L/a)가 증가할수록 세굴 깊이가 감소했습니다. 예를 들어, 뾰족한 유선형 교각의 경우 종횡비가 1에서 4로 증가했을 때 세굴 깊이는 26% 감소했습니다. 이는 교각 길이가 길어질수록 하류의 후류 와류(wake vortex)가 약화되기 때문입니다.

발견 2: ‘더 적은 것이 더 효과적이다’ – 3개 희생파일의 우수성

희생파일은 효과적인 세굴 방지책이지만, 파일의 개수와 배열이 효율성을 좌우했습니다. 놀랍게도 3개의 희생파일을 사용한 배열(Series C)이 5개를 사용한 배열(Series B)보다 더 뛰어난 세굴 감소 효과를 보였습니다.

  • 표 4.5에 따르면, 뾰족한 유선형 교각(L/a=2)의 경우, 3개 희생파일 배열은 5개 배열에 비해 24% 더 높은 세굴 감소율을 보였습니다. 이는 파일 사이의 간격이 넓어져 상류에서 발생한 세굴 퇴적물이 교각 주변으로 더 원활하게 이동 및 퇴적되어 주 교각을 보호하는 효과를 낳기 때문으로 분석됩니다. 본 연구에서 관찰된 최대 세굴 감소율은 모서리가 둥근 사각형 교각(L/a=4)에 3개의 희생파일을 적용했을 때 기록된 64%였습니다.

R&D 및 운영을 위한 실질적 시사점

  • 공정 엔지니어: 교량 설계 시, 단순히 폭이 좁은 교각보다는 종횡비가 높은 유선형 교각을 채택하는 것이 세굴을 최소화하는 데 훨씬 효과적일 수 있습니다. 이는 기초 공사 비용을 직접적으로 절감하는 요인이 됩니다.
  • 품질 관리팀: 본 연구에서 개발된 새로운 세굴 예측 공식(논문의 식 4.7)은 기존 HEC-18 공식보다 교각 형상과 종횡비의 영향을 더 정밀하게 반영합니다. 이를 활용하면 기존 교량의 세굴 위험도를 더 정확하게 평가하고, 우선순위에 따른 유지보수 계획을 수립할 수 있습니다.
  • 설계 엔지니어: 사각형과 같이 흐름 박리가 심한 형상은 피하고, 뾰족하거나 둥근 유선형 설계를 초기 단계부터 고려해야 합니다. 또한 희생파일 방지책을 설계할 때, 파일의 개수보다는 최적의 간격과 배열을 통해 흐름을 제어하고 퇴적물 이동을 유도하는 것이 더 경제적이고 효과적일 수 있습니다.

논문 상세 정보


The Role of Pier Shape and Aspect Ratio on Local Scour with and Without Sacrificial Piles

1. 개요:

  • 제목: The Role of Pier Shape and Aspect Ratio on Local Scour with and Without Sacrificial Piles (희생파일 유무에 따른 교각 형상과 종횡비가 국소 세굴에 미치는 영향)
  • 저자: Mohamed Kharbeche
  • 발표 연도: 2022
  • 발표 학회/저널: University of Windsor (석사 학위 논문)
  • 키워드: Pier shape, Aspect ratio, Local scour, Sacrificial piles, Scour reduction

2. 초록:

교각 주변의 세굴 과정은 복잡하여 비경제적인 교각 설계와 불필요한 비용을 초래합니다. 이는 현재 사용되는 세굴 예측 방법들이 세굴 깊이를 과도하게 예측하기 때문입니다. 교각 형상 및 종횡비와 같은 여러 세굴 측면은 교각 설계에서 충분히 고려되지 않아 추가적인 연구가 필요합니다. 또한, 교각을 보호하고 세굴 깊이를 줄이기 위해 세굴 방지책이 사용됩니다. 본 연구의 첫 번째 목표는 교각 선단부 형상과 종횡비의 복합적인 효과가 세굴 형상에 미치는 영향을 연구하는 것입니다. 두 번째 목표는 교각 전면에 위치한 두 가지 다른 희생파일 배열이 세굴 감소에 미치는 효과를 더 잘 이해하는 것입니다. 실험은 다양한 교각 형상과 종횡비로 수행되었습니다. 사용된 형상은 둥근 유선형, 뾰족한 유선형, 모서리가 둥근 사각형 및 사각형이며, 세 가지 종횡비(L/a = 1, 2, 4)를 가진 교각에 적용되었습니다. 또한, 두 개의 삼각형 희생파일 배열을 사용하여 희생파일이 세굴 감소에 미치는 역할을 연구했습니다. L/a = 4인 뾰족한 유선형 교각이 최소 세굴 깊이를 기록했습니다. 또한, 삼각형 배열의 세 개의 희생파일이 최대 세굴 감소를 가져왔습니다. 본 연구와 이전 실험 결과를 사용하여 새로운 세굴 예측 방법이 개발되었습니다. 박리 속도, 교각 형상 및 종횡비가 방정식에 통합되었습니다. 이러한 매개변수들은 세굴에 영향을 미치는 중요한 요인으로 조사되고 발견되었습니다.

Figure 1.1: Scour-related bridge failure in Alberta, Canada (CTV News, 2013)
Figure 1.1: Scour-related bridge failure in Alberta, Canada (CTV News, 2013)

3. 서론:

세굴은 교량, 특히 유압 공학 인프라 실패의 주요 원인 중 하나입니다. 교각 기초 주변의 퇴적물이 제거되면서 구조적 무결성이 영향을 받습니다. 북미에서는 교량 붕괴의 50% 이상이 세굴 또는 세굴 관련 문제로 인해 발생합니다. Shirhole과 Holt(1991)는 미국에서 800건 이상의 교량 붕괴를 조사했으며, 60%의 실패가 교각 주변의 하상 세굴 및 수로 불안정성과 관련이 있음을 발견했습니다. 교량 붕괴는 교체 또는 수리 비용으로 인해 추가적인 비용을 발생시킵니다. 캐나다에서도 2013년 앨버타에서 폭우로 인한 홍수로 캐나다 태평양 철도 교량이 세굴로 붕괴되는 사고가 발생했습니다. 현재 널리 사용되는 HEC-18(CSU) 방정식은 교각 형상 계수(K1)를 포함하지만, 종횡비(L/a)의 효과를 명시적으로 다루지 않아 예측에 한계가 있습니다. 따라서 본 연구는 교각 형상, 종횡비, 그리고 희생파일과 같은 세굴 방지책의 효과를 종합적으로 분석하여 보다 정확한 세굴 예측과 경제적인 설계를 위한 기초 자료를 제공하고자 합니다.

4. 연구 요약:

연구 주제의 배경:

교량 교각 주변의 국소 세굴은 교량의 안전과 수명에 직접적인 영향을 미치는 중요한 문제입니다. 현재의 설계 기준은 종종 보수적이어서 과도한 안전율을 적용하게 되고, 이는 건설 비용 증가로 이어집니다.

이전 연구 현황:

대부분의 이전 연구는 원형 교각에 초점을 맞추었으며, 사각형이나 유선형과 같은 비원형 교각, 특히 다양한 종횡비를 가진 교각에 대한 연구는 상대적으로 부족했습니다. 또한 희생파일의 효과에 대한 연구는 많았지만, 다양한 교각 형상과 결합하여 그 효율성을 체계적으로 분석한 연구는 드물었습니다.

Figure 2.1: Description of flow structures around a pier (Hodi, 2009)
Figure 2.1: Description of flow structures around a pier (Hodi, 2009)

연구 목적:

  1. 교각의 선단부 형상(round-nosed, sharp-nosed, round-edged)이 세굴 형상에 미치는 영향을 분석합니다.
  2. 교각의 종횡비(L/a)가 세굴 깊이에 미치는 영향을 조사합니다.
  3. 5개 및 3개의 희생파일을 삼각형으로 배열했을 때의 세굴 감소 효과를 탐구합니다.
  4. 본 연구 결과와 기존 문헌을 바탕으로 개선된 세굴 예측 방법을 개발합니다.

핵심 연구:

실험실 수로에서 다양한 형상과 종횡비를 가진 교각 모델을 설치하고, 통제된 유속 하에서 24시간 동안 세굴을 발생시킨 후 그 형상을 측정했습니다. 일부 실험에서는 교각 상류에 희생파일을 설치하여 방지책의 효과를 정량적으로 평가했습니다. 유동장 특성을 파악하기 위해 LDV와 ADV를 사용한 유속 측정도 병행되었습니다.

5. 연구 방법론

연구 설계:

본 연구는 세 가지 시리즈의 실험으로 구성되었습니다. – Series A: 희생파일이 없는 상태에서 10가지 다른 교각 형상 및 종횡비 조합에 대한 세굴 실험을 수행했습니다. – Series B: Series A에서 사용된 교각 중 L/a=2, 4인 교각에 5개의 희생파일을 적용하여 세굴 감소 효과를 측정했습니다. – Series C: 동일한 교각에 3개의 희생파일을 적용하여 Series B와 효과를 비교했습니다.

데이터 수집 및 분석 방법:

수집된 세굴 프로파일 데이터는 dse/a(상대 세굴 깊이)로 무차원화하여 비교 분석했습니다. 희생파일의 효과는 방지책이 없을 때의 세굴 깊이(dseo)와 있을 때의 세굴 깊이(dse)를 비교하여 세굴 감소율(rde)로 정량화했습니다. ADV로 측정한 유속 데이터는 교각 주변의 흐름 박리 속도(separation velocity)를 분석하는 데 사용되었으며, 이는 새로운 세굴 예측 공식 개발에 활용되었습니다.

연구 주제 및 범위:

본 연구는 맑은 물 세굴 조건 하에서 단일 교각 주변의 국소 세굴에 초점을 맞추었습니다. 교각의 형상, 종횡비, 그리고 희생파일의 개수 및 배열이 주요 변수입니다. 교각의 경사(skewness)나 군집 교각(pier groups)의 효과는 본 연구의 범위에 포함되지 않습니다.

6. 주요 결과:

주요 결과:

  • 교각 형상은 세굴 깊이에 큰 영향을 미칩니다. L/a=4인 뾰족한 유선형 교각은 원형 교각 대비 25%의 세굴 감소를 보인 반면, L/a=1인 사각형 교각은 66%의 세굴 증가를 보였습니다.
  • 교각의 종횡비가 증가할수록 상대 세굴 깊이(dse/a)는 감소합니다. 둥근 유선형 교각의 경우, L/a가 1에서 4로 증가하자 세굴 깊이는 21% 감소했습니다.
  • 희생파일은 효과적인 세굴 방지책이며, 3개 파일 배열이 5개 파일 배열보다 더 높은 세굴 감소율을 보였습니다. 최대 64%의 세굴 감소 효과가 관찰되었습니다.
  • 교각 형상, 종횡비, 흐름 박리 속도를 고려한 새로운 세굴 예측 공식을 개발했으며, 이 공식은 기존 HEC-18 공식보다 실험 데이터와 더 잘 일치하는 경향을 보였습니다.
Figure 4.27: Contour profiles for piers with L/a = 2 in Series B and Series C with five and three sacrificial piles (tests B5, B6, and B7 with five sacrificial piles, and tests C5, C6, and C7 with three sacrificial piles) 40
Figure 4.27: Contour profiles for piers with L/a = 2 in Series B and Series C with five and three sacrificial piles (tests B5, B6, and B7 with five sacrificial piles, and tests C5, C6, and C7 with three sacrificial piles)

Figure 목록:

  • Figure 1.1: Scour-related bridge failure in Alberta, Canada (CTV News, 2013)
  • Figure 2.1: Description of flow structures around a pier (Hodi, 2009).
  • Figure 2.2: Collar (Plan and side views) (Tafarojnoruz et al., 2012).
  • Figure 2.3: Schematic of the sacrificial piles in a transverse arrangement (Tafarojnoruz et al., 2012).
  • Figure 3.1: Schematic of the horizontal laboratory flume used for the experiments (modified from (Williams, 2019))
  • Figure 3.2: Streamwise velocity profiles in the presence and in the absence of the 3 mm rod placed in the sand bed.
  • Figure 3.3: ASTM sieve analysis for bed sediment used in the experiments
  • Figure 3.4: Point measurements of a centerline profile
  • Figure 3.5: Location of the ADV and LDV for the tests in the absence of the pier.
  • Figure 3.6: Location of the ADV for tests with 5 and 3 sacrificial piles (B6, B7, B8, C8, C9, and C10)
  • Figure 3.7: Location of the ADV for the tests (A4, A8, A9, and A10) to get the separation velocity.
  • Figure 3.8: Different pier shapes and L/a ratios.
  • Figure 3.9: Schematic of the five sacrificial piles used in Series B
  • Figure 3.10: Schematic of the three sacrificial piles used in Series C
  • Figure 4.1: Streamwise velocity U profiles for tests B6, B7, and B8 with five sacrificial piles compared to tests E and L in the absence of the pier
  • Figure 4.2: Streamwise velocity U profiles for tests C8, C9, and C10 with three sacrificial piles compared to tests E and L in the absence of the pier
  • Figure 4.3: Reynolds shear stress profiles for tests B6, B7, and B8 with five sacrificial piles compared to test E in the absence of the pier
  • Figure 4.4: Reynolds shear stress profiles for tests C8, C9, and C10 with three sacrificial piles compared to test E in the absence of the pier.
  • Figure 4.5: Centerline profiles of the piers with L/a =1 (A1, A2, A3, and A4).
  • Figure 4.6: Centerline profiles of the piers with L/a =2 (A5, A6, and A7).
  • Figure 4.7: Centerline profiles of the piers with L/a =4 (A8, A9, and A10).
  • Figure 4.8: Contour profiles of the piers with L/a =1 (A1, A2, A3, and A4)
  • Figure 4.9: Contour profiles of the piers with L/a =2 (A5, A6, and A7)
  • Figure 4.10: Contour profiles of the piers with L/a = 4 (A8, A9, and A10)
  • Figure 4.11: Centerline profiles of round-nosed piers (A1: L/a = 1, A5: L/a = 2, and A8: L/a = 4)
  • Figure 4.12: Centerline profiles of sharp-nosed piers (A2: L/a = 1, A6: L/a = 2, and A9: L/a = 4)
  • Figure 4.13:Centerline profiles of round-edged piers (A3: L/a = 1, A7: L/a = 2, and A10: L/a = 4)
  • Figure 4.14: Contour profiles of round-nosed piers (A1: L/a = 1, A5: L/a = 2, and A8: L/a = 4).
  • Figure 4.15: Contour profiles of sharp-nosed piers (A2: L/a = 1, A6: L/a = 2, and A9: L/a = 4)
  • Figure 4.16: Contour profiles of round-nosed piers (A3: L/a = 1, A7: L/a = 2, and A10: L/a = 4)
  • Figure 4.17: Centerline profiles for piers with L/a = 2 with and without five sacrificial piles (tests A5, A6, and A7 without sacrificial piles, and tests B5, B6, and B7 with five sacrificial piles)
  • Figure 4.18: Centerline profiles for piers with L/a = 4 with and without five sacrificial piles (tests A8, A9, and A10 without sacrificial piles, and tests B8, B9, and B10 with five sacrificial piles)
  • Figure 4.19: Contour profiles for piers with L/a = 2 with and without five sacrificial piles (tests A5, A6, and A7 without sacrificial piles, and tests B5, B6, and B7 with five sacrificial piles)
  • Figure 4.20: Contour profiles for piers with L/a = 4 with and without five sacrificial piles (tests A8, A9, and A10 without sacrificial piles, and tests B8, B9, and B10 with five sacrificial piles).
  • Figure 4.21: Centerline profiles for piers with L/a = 2 with and without three sacrificial piles (tests A5, A6, and A7 without sacrificial piles, and tests C5, C6, and C7 with three sacrificial piles).
  • Figure 4.22: Centerline profiles for piers with L/a = 4 with and without three sacrificial piles (tests A8, A9, and A10 without sacrificial piles, and tests C8, C9, and C10 with three sacrificial piles)
  • Figure 4.23: Contour profiles for piers with L/a = 2 with and without three sacrificial piles (tests A5, A6, and A7 without sacrificial piles, and tests C5, C6, and C7 with three sacrificial piles).
  • Figure 4.24: Contour profiles for piers with L/a = 4 with and without three sacrificial piles (tests A8, A9, and A10 without sacrificial piles, and tests C8, C9, and C10 with three sacrificial piles)
  • Figure 4.25: Centerline profiles for L/a = 2 in Series B and Series C with five and three sacrificial piles (tests: B5, B6, and B7 with five sacrificial piles, and tests C5, C6, and C7 with three sacrificial piles)
  • Figure 4.26: Centerline profiles for L/a = 4 in Series B and Series C with five and three sacrificial piles (tests: B8, B9, and B10 with five sacrificial piles, and tests C8, C9, and C10 with three sacrificial piles)
  • Figure 4.27: Contour profiles for piers with L/a = 2 in Series B and Series C with five and three sacrificial piles (tests B5, B6, and B7 with five sacrificial piles, and tests C5, C6, and C7 with three sacrificial piles)
  • Figure 4.28: Contour profiles for piers with L/a = 4 in Series B and Series C with five and three sacrificial piles (tests B8, B9, and B10 with five sacrificial piles, and tests C8, C9, and C10 with three sacrificial piles)
  • Figure 4.30: Separation velocity profiles for different pier shapes and L/a ratios.
  • Figure 4.30: Equilibrium scour depth alteration with L/a
  • Figure 4.31: Measured vs predicted dse/a values grouped by investigation using Equation 4.7.
  • Figure 4.32: Measured vs predicted dse/a values grouped by investigation using HEC-18 equation

7. 결론:

본 연구는 교각의 형상과 종횡비가 국소 세굴에 미치는 영향을 체계적으로 규명했습니다. – 교각 형상 및 종횡비: 뾰족한 유선형 교각과 높은 종횡비가 세굴을 최소화하는 반면, 사각형 교각은 세굴을 크게 증가시킵니다. 세굴 깊이는 종횡비가 증가함에 따라 감소하는 경향을 보입니다. – 세굴 방지책: 희생파일은 효과적인 방지책이며, 3개 파일 배열이 5개 파일 배열보다 더 효율적일 수 있습니다. 종횡비가 높은 교각일수록 희생파일의 세굴 감소 효과도 증가했습니다. – 새로운 예측 모델: 교각 형상과 종횡비, 그리고 흐름 박리 속도를 통합한 새로운 세굴 예측 모델은 기존 모델보다 더 정확한 예측을 제공할 가능성을 보여주었습니다. 이러한 결과들은 교량 설계 시 더 안전하고 경제적인 결정을 내리는 데 중요한 공학적 통찰력을 제공합니다.

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전문가 Q&A: 자주 묻는 질문

Q1: 왜 실제 하천의 ‘유사 이동 조건(live-bed)’이 아닌 ‘맑은 물 세굴(clear-water)’ 조건에서 실험을 수행했나요?

A1: 맑은 물 세굴 조건은 상류에서 퇴적물이 공급되지 않는 상태로, 교각 주변에서 발생할 수 있는 최대 잠재 세굴 깊이를 평가하는 데 사용됩니다. 이 조건은 교량 설계 시 가장 보수적이고 안전한 기준을 설정하는 데 필수적입니다. 따라서 본 연구에서는 다양한 교각 형상과 방지책의 성능을 극한 조건에서 비교 평가하기 위해 이 방법을 선택했습니다.

Q2: 5개보다 3개의 희생파일이 더 효과적인 물리적 메커니즘은 무엇인가요?

A2: 이는 파일 사이의 간격과 관련이 있습니다. 5개 파일 배열은 간격이 좁아 흐름을 강하게 막는 ‘장벽’처럼 작용하여 파일 바로 앞에서 강한 세굴을 유발할 수 있습니다. 반면, 3개 파일 배열은 간격이 더 넓어 흐름을 완전히 막기보다는 적절히 분산시키고 약화시킵니다. 이로 인해 희생파일 주변에서 발생한 퇴적물이 하류의 주 교각 주변으로 더 효과적으로 이동 및 퇴적되어, 주 교각의 기초를 보호하는 ‘자연적인 방어막’을 형성하는 데 더 유리했던 것으로 분석됩니다.

Q3: 새로 제안된 세굴 예측 공식은 기존 HEC-18 표준과 비교하여 어떤 점이 개선되었나요?

A3: HEC-18 공식은 주로 교각 폭과 유속에 의존하며, 교각 형상을 단일 보정 계수(K1)로 단순화합니다. 하지만 본 연구에서 제안된 새로운 공식(식 4.7)은 여기에 더해 교각 종횡비(L/a)와 흐름 박리 속도(separation velocity)를 반영하는 새로운 무차원수(Fds)를 도입했습니다. 이는 세굴의 주원인인 말굽 와류의 강도에 직접적인 영향을 미치는 물리적 현상을 더 정밀하게 모델링하여, 특히 유선형이나 종횡비가 큰 교각에 대해 기존 공식보다 더 정확한 예측을 제공할 수 있습니다.

Q4: 교각의 종횡비(L/a)가 증가하면 왜 세굴이 감소하나요?

A4: 교각의 종횡비가 증가하면, 즉 교각이 흐름 방향으로 길어지면, 교각 측면을 따라 흐르는 물의 흐름이 더 안정화되고 흐름 박리 지점이 하류로 이동합니다. 이는 교각 바로 뒤에 형성되는 후류 와류(wake vortices)의 강도와 주기적인 와류 방출(vortex shedding)을 약화시키는 효과를 가져옵니다. 후류 와류 역시 세굴에 기여하는 요인이므로, 이것이 약화되면 교각 하류의 세굴이 줄어들고 전반적인 세굴 구멍의 크기가 감소하게 됩니다.

Q5: 흐름 박리 속도(separation velocity)를 측정한 이유는 무엇인가요?

A5: 흐름 박리 속도는 교각 측면에서 흐름이 표면에서 떨어져 나가기 시작하는 지점의 속도로, 세굴을 일으키는 가장 강력한 메커니즘인 말굽 와류의 형성과 강도에 직접적인 영향을 미칩니다. 본 연구에서는 교각 형상에 따라 이 박리 지점과 속도가 어떻게 변하는지를 측정함으로써(그림 4.29 참조), 각기 다른 형상이 왜 다른 세굴 깊이를 보이는지에 대한 물리적 근거를 파악했습니다. 이 데이터는 더 정확한 세굴 예측 모델을 개발하는 데 핵심적인 역할을 했습니다.


결론: 더 높은 품질과 생산성을 위한 길

교량 세굴은 피할 수 없는 자연 현상이지만, 그 영향을 최소화하는 것은 공학 기술에 달려 있습니다. 본 연구는 교각의 형상을 유선형으로 설계하고 종횡비를 높이는 것만으로도 세굴을 크게 줄일 수 있으며, 희생파일과 같은 방지책은 ‘많이’ 설치하는 것보다 ‘어떻게’ 배열하는지가 더 중요하다는 실질적인 증거를 제시합니다. 이러한 통찰력은 더 안전하고 경제적인 교량 설계를 가능하게 합니다.

STI C&D는 최신 산업 연구 결과를 적용하여 고객이 더 높은 생산성과 품질을 달성할 수 있도록 돕는 데 전념하고 있습니다. 이 논문에서 논의된 과제가 귀사의 운영 목표와 일치한다면, 저희 엔지니어링 팀에 연락하여 이러한 원칙을 귀사의 구성 요소에 어떻게 구현할 수 있는지 알아보십시오.

(주)에스티아이씨앤디에서는 고객이 수치해석을 직접 수행하고 싶지만 경험이 없거나, 시간이 없어서 용역을 통해 수치해석 결과를 얻고자 하는 경우 전문 엔지니어를 통해 CFD consulting services를 제공합니다. 귀하께서 당면하고 있는 연구프로젝트를 최소의 비용으로, 최적의 해결방안을 찾을 수 있도록 지원합니다.

  • 연락처 : 02-2026-0442
  • 이메일 : flow3d@stikorea.co.kr

저작권 정보

  • 이 콘텐츠는 Mohamed Kharbeche의 논문 “The Role of Pier Shape and Aspect Ratio on Local Scour with and Without Sacrificial Piles”를 기반으로 한 요약 및 분석 자료입니다.
  • 출처: https://scholar.uwindsor.ca/etd/8791

이 자료는 정보 제공 목적으로만 사용됩니다. 무단 상업적 사용을 금지합니다. Copyright © 2025 STI C&D. All rights reserved.

Figure 3. Schematic diagram for calculation of maximum scour depth.

극한 홍수에도 안전한 교량 설계: 최대 교량 세굴 깊이 종합 계산법

이 기술 요약은 Rupayan Saha, Seung Oh Lee, Seung Ho Hong이 2018년 ‘water’ 저널에 발표한 논문 “A Comprehensive Method of Calculating Maximum Bridge Scour Depth”를 기반으로 하며, STI C&D가 기술 전문가를 위해 분석하고 요약했습니다.

키워드

  • Primary Keyword: 교량 세굴 깊이
  • Secondary Keywords: 교량 세굴, 퇴적물 이송, 잠김 흐름, 수리 모형 실험, CFD, 교량 안전

Executive Summary

  • 문제점: 기존의 교량 세굴 깊이 산정 공식은 극한 기상 현상으로 인한 교각 월류(overtopping)나 잠김 흐름(submerged flow)과 같은 복잡한 유동 조건을 정확히 반영하지 못하며, 국부 세굴과 수축 세굴을 독립적인 현상으로 간주하여 예측 정확도가 떨어집니다.
  • 연구 방법: 실제 하천(Towaliga River)의 지형을 1:60으로 축소한 복단면 수로 수리 모형을 제작하고, 자유 수면 흐름, 잠김 오리피스 흐름, 월류 흐름 등 다양한 조건에서 세굴 실험을 수행했습니다.
  • 핵심 발견: 최대 세굴 깊이는 ‘이론적 교각 세굴’과 ‘흐름 수축에 의한 추가 세굴’의 합으로 구성된다는 가설을 세우고, 추가 세굴량이 유량 수축비와 명확한 상관관계가 있음을 실험적으로 증명했습니다.
  • 핵심 결론: 본 연구는 복잡한 흐름 조건에서도 최대 교량 세굴 깊이를 더 정확하게 예측할 수 있는 통합적이고 포괄적인 방법을 제시하여, 교량의 구조적 안전성 설계를 크게 향상시킬 수 있습니다.

문제점: CFD 전문가에게 이 연구가 중요한 이유

교량 붕괴의 가장 큰 원인은 교량 기초 주변의 하상 재료가 유실되는 ‘세굴’ 현상입니다. 미국에서는 1950년 이후 발생한 교량 붕괴의 약 60%가 세굴과 관련 있을 정도로 교량 안전에 치명적입니다. 특히 최근 빈번해지는 극한 기상 현상은 설계 기준을 초과하는 홍수를 유발하며 교량의 안전을 심각하게 위협합니다.

기존의 세굴 깊이 예측 공식들은 대부분 단순화된 사각 수로에서의 자유 수면 흐름 실험을 기반으로 개발되었습니다. 이로 인해 실제 하천의 불규칙한 지형이나, 극한 홍수 시 발생하는 교량 상판 월류 및 잠김 흐름과 같은 복잡한 수리 현상을 제대로 모사하지 못하는 한계가 있습니다. 또한, 현재 설계 실무에서는 흐름 단면 축소로 인한 ‘수축 세굴’과 교각 주변의 와류로 인한 ‘국부 세굴’을 별개의 현상으로 보고 각각 계산한 뒤 합산하지만, 실제로는 두 현상이 동시에 상호작용하며 발생하기 때문에 예측에 오차가 발생합니다. 이러한 부정확성은 교량 설계의 과잉 또는 과소 평가로 이어져 비경제적이거나 위험한 결과를 초래할 수 있습니다.

Figure 1. Towaliga River bridge in the field and model in the laboratory.
Figure 1. Towaliga River bridge in the field and model in the laboratory.

연구 접근법: 방법론 분석

본 연구는 이러한 한계를 극복하기 위해 미국 조지아주 메이컨에 위치한 Towaliga 강 교량을 대상으로 1:60 축척의 정밀한 물리적 수리 모형을 제작했습니다. 이 모형은 실제 하천의 복잡한 지형(복단면 형상)을 그대로 재현했으며, 세굴 실험을 위해 중앙부에 이동상(mobile bed) 구간을 설치하고 0.53mm의 중간 입경(d50)을 가진 모래를 사용했습니다.

연구팀은 다양한 홍수 시나리오를 모사하기 위해 세 가지 주요 흐름 조건에서 실험을 수행했습니다. 1. 자유 수면 흐름 (Free Flow): 일반적인 홍수 조건 2. 잠김 오리피스 흐름 (Submerged Orifice Flow): 수위가 교량 상판 하단까지 상승한 조건 3. 월류 흐름 (Overtopping Flow): 수위가 교량 상판을 넘어 흐르는 극한 홍수 조건

각 실험에서 유량과 수위를 정밀하게 제어했으며, 세굴이 평형 상태에 도달할 때까지 5~6일간 실험을 지속했습니다. 세굴 전후의 하상 고도는 음향 도플러 유속계(Acoustic Doppler Velocimeter, ADV)와 포인트 게이지를 사용하여 상세하게 측정되었고, 이를 통해 최대 세굴 깊이와 위치를 정확하게 파악했습니다.

핵심 발견: 주요 결과 및 데이터

연구팀은 실험 결과를 분석하여 기존 세굴 예측 방식의 한계를 극복할 새로운 종합적 방법을 제안했습니다.

결과 1: 최대 세굴 깊이의 새로운 구성 = 이론적 세굴 + 흐름 수축에 의한 추가 세굴

본 연구는 최대 세굴 깊이가 기존의 이론적 교각 세굴 깊이(CSU 또는 M/S 공식으로 계산)에 ‘흐름 수축으로 인한 추가적인 세굴 깊이’가 더해진 결과라는 핵심적인 가설을 제시했습니다. 실험 데이터를 분석한 결과, 이 ‘추가 세굴’ 성분은 교량을 통과하는 흐름의 수축 정도를 나타내는 ‘유량 수축비(q2/q1)’와 매우 강한 양의 상관관계를 보였습니다. 그림 4에서 볼 수 있듯이, 유량 수축비가 증가함에 따라 추가 세굴 깊이(Ym-csu/Y1)가 선형적으로 증가하는 경향이 뚜렷하게 나타났습니다. 이는 흐름이 교량 구간에서 더 많이 압축될수록 세굴이 더 심각해진다는 것을 정량적으로 입증한 것입니다.

결과 2: 압력 흐름 조건에서 세굴 효과 증폭

그림 4의 데이터는 또 다른 중요한 사실을 보여줍니다. 자유 수면 흐름(F)에 비해 잠김 오리피스 흐름(SO)이나 월류 흐름(OT)과 같은 압력 흐름(Pressure Flow) 조건에서 유량 수축비 증가에 따른 추가 세굴 깊이의 증가율(그래프의 기울기)이 훨씬 더 가파릅니다. 이는 압력 흐름 조건에서는 기존의 수평적 흐름 수축뿐만 아니라 교량 상판에 의한 수직적 흐름 수축이 추가로 발생하여 유속이 더 크게 증가하고, 결과적으로 세굴 현상이 증폭되기 때문입니다. 이는 극한 홍수 시 교량 안전성 평가에 반드시 고려해야 할 핵심 요소입니다.

R&D 및 운영을 위한 실질적 시사점

이 연구 결과는 교량 설계 및 안전 관리 분야의 전문가들에게 다음과 같은 실질적인 시사점을 제공합니다.

  • 수리 및 교량 설계 엔지니어: 본 연구에서 제안된 5단계 최대 세굴 깊이 예측 절차(현장 데이터 수집 → 흐름 변수 계산 → 이론적 교각 세굴 계산 → 흐름 수축에 따른 추가 세굴 추정 → 합산)는 기존 방식보다 훨씬 더 정확하고 신뢰성 있는 교량 기초 설계를 가능하게 합니다. 특히 극한 홍수 조건에 대한 안전성을 크게 향상시킬 수 있습니다.
  • 위험 평가팀: 압력 흐름(월류 등)이 세굴을 크게 증폭시킨다는 그림 4의 결과는, 100년 또는 500년 빈도의 극한 홍수 시 월류 가능성이 있는 기존 교량들의 안전성을 재평가해야 할 필요성을 강력하게 시사합니다.
  • CFD 모델링 전문가: 이 연구에서 측정된 복잡한 흐름 조건(잠김, 월류) 하의 상세한 실험 데이터는 교량 세굴에 대한 수치 모델링(CFD)의 정확도를 검증하고 개선하는 데 매우 귀중한 자료로 활용될 수 있습니다.

논문 상세 정보


A Comprehensive Method of Calculating Maximum Bridge Scour Depth

1. 개요:

  • 제목: A Comprehensive Method of Calculating Maximum Bridge Scour Depth (최대 교량 세굴 깊이 계산을 위한 종합적 방법)
  • 저자: Rupayan Saha, Seung Oh Lee, Seung Ho Hong
  • 발표 연도: 2018
  • 발표 저널/학회: water
  • 키워드: bridge scour; sediment transport; submerged flow; physical hydraulic modeling

2. 초록:

최근 극한 기상 현상의 반복적인 발생으로 교량 주변의 세굴 문제가 두드러지고 있습니다. 따라서 교량은 이러한 극한 기상 현상 동안 겪을 수 있는 높은 유량에 대한 세굴로 인한 붕괴를 방지하기 위해 적절한 보호 조치를 갖추어 설계되어야 합니다. 그러나 여러 권장 공식에 의한 현재의 세굴 깊이 추정은 높은 유량에서 부정확한 결과를 보여줍니다. 한 가지 가능한 이유는 현재의 세굴 공식이 자유 표면 흐름을 이용한 실험에 기반하고 있지만, 극한 홍수 사건은 잠김 오리피스 흐름과 결합된 교량 월류 흐름을 유발할 수 있다는 점입니다. 또 다른 가능한 이유는 최대 세굴 깊이에 대한 현재의 관행이 국부 세굴과 수축 세굴과 같은 다른 유형의 세굴 간의 상호작용을 무시한다는 점인데, 실제로는 이러한 과정들이 동시에 발생합니다. 본 논문에서는 축소된 교량 모델을 사용하여 복합 단면 수로에서 다양한 흐름 조건(자유, 잠김 오리피스, 월류 흐름) 하에 실험실 실험을 수행했습니다. 실험실 실험 결과와 널리 사용되는 경험적 세굴 추정 방법을 결합하여, 다른 세굴 깊이의 개별적 추정과 다른 세굴 구성 요소의 상호작용에 관한 문제를 극복하는 최대 세굴 깊이를 예측하는 포괄적인 방법을 제안합니다. 또한, 최대 세굴 깊이에 대한 교각 벤트(교대에 가깝게 위치)의 존재 효과도 분석 중에 조사되었습니다. 결과는 최대 세굴 깊이의 위치는 교각 벤트의 존재와 무관하지만, 최대 세굴 깊이의 양은 교각 벤트가 있을 때보다 없을 때 유량 재분배로 인해 상대적으로 더 높다는 것을 보여줍니다.

3. 서론:

교량이 강에 건설되면, 교각과 교대 주변에 국부적으로 독특한 유동장이 발달하기 때문에 교량 주변의 흐름 패턴이 바뀝니다. 또한, 강 양쪽 또는 한쪽에 있는 제방/교대로 인해 흐름 면적이 줄어들어 가속으로 인한 유속이 빨라집니다. 더 높은 속도를 가진 이 독특한 유동장은 교량 기초에 심각한 손상을 줄 수 있습니다. 따라서 기초의 깊이가 충분히 깊지 않으면 교량 붕괴의 가능성이 높아집니다. 교량은 지진, 바람, 홍수 등 여러 원인으로 붕괴될 수 있습니다. 그중에서도 교량 세굴은 교량 붕괴의 가장 큰 원인입니다. 예를 들어, 1950년 이후 미국에서 발생한 전체 교량 붕괴 중 약 60%가 교량 기초의 세굴과 관련이 있습니다. 콜로라도 교통부(CDOT)는 2013년 홍수로 최소 30개의 주 고속도로 교량이 파괴되고 20개가 심각하게 손상되었다고 추정했습니다. 네팔에서는 2014년 홍수 동안 하상 재료의 퇴화로 인해 티나우 강 위의 고속도로 교량 기초가 심각하게 노출되었습니다. 위 예에서 설명한 바와 같이, 교량 세굴은 전 세계적으로 주요 교량 안전 문제 중 하나라고 말하는 것이 정당합니다. 따라서 교량 기초에서의 정확한 세굴 예측은 교량 안전을 위한 엔지니어의 주요 목표가 됩니다.

4. 연구 요약:

연구 주제의 배경:

교량 세굴은 교량 붕괴의 주된 원인으로, 특히 극한 홍수 시 그 위험성이 커집니다. 기존의 세굴 예측 공식은 실제 하천의 복잡한 흐름 조건과 세굴 메커니즘의 상호작용을 제대로 반영하지 못해 정확도에 한계가 있었습니다.

이전 연구 현황:

1950년대 후반부터 수많은 연구가 진행되어 평형 세굴 깊이 추정 공식이 개발되었습니다. 그러나 대부분의 연구는 단순화된 직사각형 수로와 자유 수면 흐름 조건에서 수행되었습니다. 또한, 국부 세굴과 수축 세굴을 독립적인 과정으로 가정하여 각각을 계산 후 합산하는 방식을 사용해왔습니다.

연구 목적:

본 연구의 주된 목적은 다양한 유형의 세굴이 동시에 발생하는 상황에서 최대 세굴 깊이를 예측하는 데 사용할 수 있는 단일 방정식을 개발하는 것입니다. 이를 위해 서로 다른 세굴 구성 요소 간의 상호 작용을 규명하고, 널리 사용되는 세굴 공식(CSU, M/S)과 비교하여 최대 세굴 깊이를 계산하는 개선된 방법을 제안하고자 합니다.

핵심 연구:

실제 하천 지형을 모사한 1:60 축소 수리 모형을 이용하여 자유 흐름, 잠김 오리피스 흐름, 월류 흐름 조건에서 실험을 수행했습니다. 실험을 통해 측정한 최대 세굴 깊이와 기존 이론 공식을 비교 분석하여, ‘이론적 교각 세굴’과 ‘흐름 수축에 의한 추가 세굴’의 합으로 최대 세굴 깊이를 표현하는 새로운 접근법을 제시하고, 그 유효성을 검증했습니다.

5. 연구 방법론

연구 설계:

본 연구는 실제 교량(Towaliga River bridge)의 1:60 축소 물리 모형을 이용한 실험적 접근법을 채택했습니다. 복단면 형상의 수로에 이동상 구간을 설치하고, 다양한 수리 조건(자유 흐름, 잠김 오리피스 흐름, 월류 흐름)을 재현하여 세굴 현상을 관찰하고 측정했습니다.

데이터 수집 및 분석 방법:

  • 하상 변동 측정: 음향 도플러 유속계(ADV)와 포인트 게이지를 사용하여 실험 전후의 하상 고도를 정밀하게 측정하고, 이를 통해 세굴 깊이와 범위를 분석했습니다.
  • 유속 측정: ADV를 사용하여 접근부 및 교량 단면에서 3차원 유속 분포를 측정했습니다.
  • 데이터 분석: 측정된 유량, 수위, 유속, 세굴 깊이 등의 변수를 사용하여 기존 세굴 공식(CSU, M/S)과 본 연구에서 제안한 새로운 모델을 비교 분석했습니다. 특히, ‘추가 세굴 깊이’와 ‘유량 수축비’ 간의 상관관계를 회귀 분석을 통해 도출했습니다.
Figure 3. Schematic diagram for calculation of maximum scour depth.
Figure 3. Schematic diagram for calculation of maximum scour depth.

연구 주제 및 범위:

  • 주요 연구 주제: 복잡한 흐름 조건(특히 압력 흐름)에서 발생하는 최대 교량 세굴 깊이의 종합적인 예측 방법 개발.
  • 연구 범위: 단일 교량을 대상으로 한 축소 모형 실험에 국한됩니다. 실험은 청수 세굴(clear-water scour) 조건에서 수행되었으며, 퇴적물 입경은 0.53mm로 고정되었습니다. 교각 벤트의 유무에 따른 영향을 질적으로 분석했습니다.

6. 주요 결과:

주요 결과:

  • 최대 세굴 깊이는 이론적 교각 세굴 깊이와 흐름 수축에 의한 추가 세굴 깊이의 합으로 표현될 수 있습니다.
  • 흐름 수축에 의한 추가 세굴 깊이는 유량 수축비(q2/q1)와 강한 양의 상관관계를 가집니다. 즉, 유량 수축비가 클수록 추가 세굴이 더 깊어집니다.
  • 압력 흐름(잠김 및 월류) 조건에서는 자유 수면 흐름 조건에 비해 추가 세굴 효과가 더 크게 나타납니다. 이는 수직 흐름 수축이 추가되기 때문입니다.
  • 최대 세굴 깊이의 발생 위치는 인접한 교각의 유무와 무관하지만, 인접 교각이 없을 경우 유량 재분배로 인해 최대 세굴 깊이가 약간 더 깊어지는 경향을 보입니다.
  • 기존 공식 중 CSU 공식이 M/S 공식보다 동일 조건에서 더 큰 세굴 깊이를 예측하며, 이는 M/S 공식이 청수 세굴 조건을 고려하는 유속 강도 인자(V2/Vc)를 포함하기 때문입니다.
Table 2. Summary of experimental results to calculate maximum scour depth.
Table 2. Summary of experimental results to calculate maximum scour depth.

그림 목록:

  • Figure 1. Towaliga River bridge in the field and model in the laboratory.
  • Figure 2. Geometry of compound channel for (a) plan view with velocity measurement locations; (b) cross section view at bridge.
  • Figure 3. Schematic diagram for calculation of maximum scour depth.
  • Figure 4. Effect of flow contraction on additional scour components using (a) Colorado State University (CSU) and (b) Melville-Sheppard (M/S) equations.
  • Figure 5. Comparison of CSU and M/S pier scour depth in terms of flow intensity.
  • Figure 6. Comparison of cross-sections for runs 3 and 8.

7. 결론:

많은 연구가 교량 교각 주변의 최대 세굴 깊이를 추정하고 세굴 메커니즘을 이해하기 위해 이루어졌습니다. 대부분의 이전 연구는 자유 흐름 하의 직사각형 수로를 사용한 실험실 실험에 기반했습니다. 그러나 최근의 극한 강우 사건으로 인해 교량에서는 잠김 오리피스 흐름과 월류 흐름이 빈번하게 발생하며, 이때 교량 하부 구조 주변의 유동장은 기존의 측면 흐름 수축에 더해 수직 흐름 수축 때문에 자유 흐름보다 더 복잡합니다. 또한, 대부분의 자연 하천 형태는 직사각형이 아닙니다. 현재 HEC-18에서 권장하는 지침은 수축 세굴과 국부 세굴 과정이 독립적이어서 별도로 결정하고 합산하여 총 세굴 깊이를 추정할 수 있다고 가정했습니다. 그러나 대규모 홍수 사건 동안 국부 세굴과 수축 세굴은 동시에 발생하며, 국부 세굴과 수축 세굴을 별도로 계산하면 부정확한 세굴 깊이를 초래합니다. 현재 방법론이 가진 약점을 극복하기 위해, 축소된 물리적 모델에서 실험실 실험을 수행하고 압력 흐름뿐만 아니라 자유 흐름 사례에서도 다른 유형의 세굴 구성 요소를 별도로 계산하지 않고 사용할 수 있는 최대 세굴 깊이를 예측하기 위한 단일 방정식이 개발되었습니다.

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  35. Melville, B.W. Pier and abutment scour: Integrated approach. J. Hydraul. Eng. 1997, 123, 125–136.

전문가 Q&A: 자주 묻는 질문

Q1: 일반적인 사각 수로가 아닌 특정 강(Towaliga River)의 1:60 축소 모형을 사용한 이유는 무엇인가요?

A1: 실제 하천은 본류와 홍수터로 구성된 복단면 형상과 불규칙한 지형을 가지고 있습니다. 단순화된 사각 수로는 이러한 복잡성을 재현할 수 없습니다. 실제 하천 지형을 그대로 모사함으로써, 본 연구의 결과가 이상적인 실험실 조건을 넘어 실제 현장에 더 가깝게 적용될 수 있도록 신뢰도를 높이기 위함입니다.

Q2: 그림 4에서 자유 흐름과 압력 흐름의 추세선 기울기가 다르게 나타나는 물리적 이유는 무엇인가요?

A2: 압력 흐름(잠김 및 월류) 조건에서는 교량 상판으로 인해 흐름이 수직 방향으로도 압축됩니다. 이는 기존의 수평적 흐름 수축에 더해 추가적인 유속 증가를 유발합니다. 따라서 동일한 유량 수축비(q2/q1)에서도 압력 흐름 조건일 때 ‘추가 세굴’ 효과가 더 크게 나타나 그래프의 기울기가 더 가파르게 되는 것입니다.

Q3: 논문에서 비교한 CSU 공식과 M/S 공식 중, M/S 공식이 지속적으로 더 낮은 세굴 깊이를 예측하는 이유는 무엇인가요? (그림 5 참조)

A3: M/S 공식은 유속과 한계유속의 비(V2/Vc)인 ‘유속 강도 인자’를 포함하여 청수 세굴(clear-water scour) 조건을 고려합니다. 반면, CSU 공식은 주로 이동상 세굴(live-bed scour)을 기반으로 개발되어 이 인자를 1로 가정합니다. 본 연구는 청수 세굴 조건에서 수행되었으므로, M/S 공식이 유속 강도 인자를 반영하여 CSU 공식보다 더 낮은 세굴 깊이를 예측하게 됩니다.

Q4: 실험 7과 8에서 교각 #7을 제거한 것의 의미는 무엇인가요?

A4: 이는 교각 간의 상호작용과 인접한 교각의 존재가 최대 세굴 깊이에 미치는 영향을 질적으로 분석하기 위함이었습니다. 실험 결과, 최대 세굴이 발생하는 ‘위치’는 교각 #7의 유무와 상관없이 교각 #6에서 동일했습니다. 하지만 최대 세굴의 ‘깊이’는 교각 #7이 없을 때 유량 재분배 현상으로 인해 약간 더 깊게 나타났습니다.

Q5: 이 연구에서 ‘흐름 수축에 의한 추가 세굴’은 어떻게 정의되고 계산되었나요?

A5: 이는 측정된 총 최대 세굴 깊이에서 표준 이론적 교각 세굴 공식으로 설명되지 않는 부분을 의미합니다. 구체적으로, 세굴이 가장 깊은 지점의 총 수심(Ym)에서 CSU 공식(dcsu) 또는 M/S 공식(dms)으로 계산된 이론적 교각 세굴 깊이를 빼서 계산했습니다. 이는 논문의 식 (7)과 (8)에 명시되어 있습니다.


결론: 더 높은 품질과 생산성을 위한 길

기존의 교량 세굴 깊이 예측 방법은 극한 홍수와 같은 복잡한 실제 상황을 제대로 반영하지 못하는 명백한 한계를 가지고 있었습니다. 본 연구는 ‘이론적 세굴’과 ‘흐름 수축에 의한 추가 세굴’을 결합하는 포괄적인 접근법을 제시함으로써 이 문제를 해결하는 중요한 돌파구를 마련했습니다. 특히 압력 흐름 조건에서 세굴이 증폭된다는 사실을 정량적으로 밝혀내어, 교량 설계 및 안전 진단의 정확성을 한 차원 높일 수 있는 실질적인 통찰력을 제공합니다.

(주)에스티아이씨앤디에서는 고객이 수치해석을 직접 수행하고 싶지만 경험이 없거나, 시간이 없어서 용역을 통해 수치해석 결과를 얻고자 하는 경우 전문 엔지니어를 통해 CFD consulting services를 제공합니다. 귀하께서 당면하고 있는 연구프로젝트를 최소의 비용으로, 최적의 해결방안을 찾을 수 있도록 지원합니다.

  • 연락처 : 02-2026-0442
  • 이메일 : flow3d@stikorea.co.kr

저작권 정보

  • 이 콘텐츠는 “Rupayan Saha” 외 저자의 논문 “A Comprehensive Method of Calculating Maximum Bridge Scour Depth”를 기반으로 한 요약 및 분석 자료입니다.
  • 출처: https://doi.org/10.3390/w10111572

이 자료는 정보 제공 목적으로만 사용됩니다. 무단 상업적 사용을 금합니다. Copyright © 2025 STI C&D. All rights reserved.

Figure 3. b = 140 mm, d50 = 0.80 mm, b/d50 = 175, U/Uc = 0.95

광폭 교량 교각 세굴 심도 예측: 퇴적물 조도 효과 모델링을 통한 구조 안정성 향상

이 기술 요약은 Nordila, Ahmad 외 저자가 2017년 Pertanika J. Sci. & Technol.에 발표한 논문 “Modelling the Effect of Sediment Coarseness on Local Scour at Wide Bridge Piers”를 기반으로 하며, 기술 전문가를 위해 (주)에스티아이씨앤디 분석하고 요약했습니다.

Keywords

  • Primary Keyword: 교량 교각 세굴
  • Secondary Keywords: 퇴적물 조도, 국부 세굴, 광폭 교각, 수리 실험, CFD 토목 공학

Executive Summary

  • The Challenge: 기존의 교각 세굴 예측 공식은 광폭 교각(wide bridge piers)의 세굴 심도를 과대평가하여 불필요하고 비용이 많이 드는 기초 공사나 대책을 야기하는 경향이 있었습니다.
  • The Method: 균일한 퇴적물(입경 0.23mm, 0.80mm)로 채워진 50m 길이의 대형 수조(flume)에서 다양한 폭(0.06m ~ 0.165m)의 원통형 교각 모델을 사용하여 국부 세굴 현상을 물리적으로 모델링했습니다.
  • The Key Breakthrough: 교각 폭과 퇴적물 입경의 비율(b/d50, 퇴적물 조도)이 세굴 심도에 미치는 영향을 정량적으로 분석하여, 이 비율이 증가할수록 상대적 세굴 심도(ds/b)가 감소하는 경향을 확인하고 새로운 예측 방정식을 제안했습니다.
  • The Bottom Line: 본 연구는 퇴적물 조도를 핵심 변수로 고려하여 광폭 교각의 세굴 심도를 더 정확하게 예측할 수 있는 방정식을 제공함으로써, 교량 설계의 경제성과 안전성을 동시에 향상시킬 수 있는 길을 열었습니다.
Table 1 Summary of experimental results for the present study
Table 1 Summary of experimental results for the present study

The Challenge: Why This Research Matters for CFD Professionals

교량의 안전성은 교각 주변의 국부 세굴(local scour) 현상에 크게 좌우됩니다. 특히 유속이 느리고 수심이 얕은 곳에 설치되는 광폭 교각의 경우, 기존의 경험적 세굴 예측 공식들이 실제보다 세굴 깊이를 과대평가하는 문제가 지속적으로 제기되어 왔습니다. 이는 실험실 데이터에 기반한 공식들이 대형 구조물에 그대로 적용될 때 발생하는 오차 때문입니다. 이러한 과대 예측은 교량 기초 공사에 불필요한 비용을 발생시키고, 과도한 보강 대책을 수립하게 만드는 원인이 됩니다. 따라서 실제 현상에 더 가까운, 특히 퇴적물의 특성을 고려한 정밀한 세굴 예측 모델의 개발은 토목 및 수리 공학 분야의 중요한 과제였습니다.

The Approach: Unpacking the Methodology

본 연구는 말레이시아 국립수리연구소(NAHRIM)의 대규모 수리 실험 시설을 활용하여 수행되었습니다. 실험의 핵심 내용은 다음과 같습니다.

  • 실험 장비: 길이 50.0m, 폭 1.5m, 깊이 2.0m의 대형 수조(flume)를 사용했으며, 중앙에는 0.4m 깊이의 퇴적물 구간을 설치했습니다.
  • 퇴적물 조건: 두 종류의 균일한 무점착성 퇴적물을 사용했습니다. 중간 입경(d50)은 각각 0.23mm와 0.80mm였으며, 이는 상대적으로 고운 퇴적물과 거친 퇴적물을 대표합니다.
  • 교각 모델: 직경이 0.06m, 0.076m, 0.102m, 0.140m, 0.165m인 5개의 원통형 교각 모델을 사용하여 교각 폭의 영향을 평가했습니다.
  • 흐름 조건: 모든 실험은 퇴적물 입자가 움직이기 시작하는 한계 유속(Critical velocity, Uc)에 가까운 유속(U/Uc ≈ 0.95)의清水(clear-water) 조건에서 수행되었습니다. 이는 세굴이 주로 교각 주변의 흐름 변화에 의해 발생하는 조건을 모사한 것입니다.

연구팀은 이러한 통제된 조건 하에서 각 교각 모델과 퇴적물 조합에 따른 세굴 구멍의 시간적 발달 과정과 최종 평형 세굴 심도를 정밀하게 측정했습니다.

The Breakthrough: Key Findings & Data

실험을 통해 퇴적물 조도(sediment coarseness, b/d50)가 광폭 교각의 세굴 발달 및 최종 깊이에 미치는 영향에 대한 중요한 발견을 도출했습니다.

Finding 1: 세굴 발달의 3단계 과정 확인

본 연구는 유속 강도 U/Uc = 0.95 조건에서 세굴 발달이 뚜렷한 3단계, 즉 (i) 초기 단계, (ii) 주 침식 단계, (iii) 평형 단계를 거치는 것을 확인했습니다. 특히 주 침식 단계에서 퇴적물 조도(b/d50) 값에 따라 두 가지 다른 침식 양상이 관찰되었습니다.

  • 고운 퇴적물 (b/d50 > 230): 교각 전면의 강한 하강류(downflow)로 인해 세굴이 깊어집니다. 하강류가 세굴 구멍 바닥에 부딪히며 말굽 와류(horseshoe vortex)를 형성하고, 이 와류의 강도가 세굴 깊이에 따라 변화하며 침식 영역의 범위가 조절되는 현상이 관찰되었습니다.
  • 거친 퇴적물 (b/d50 < 230): 상대적으로 퇴적물 입자가 커서 하강류에 의한 침식이 덜 활발하며, 최종 세굴 깊이도 더 얕게 형성되었습니다.

Finding 2: 퇴적물 조도(b/d50)와 평형 세굴 심도의 관계 정립

연구의 가장 핵심적인 결과는 퇴적물 조도(b/d50)와 무차원 평형 세굴 심도(ds/b) 사이의 관계를 명확히 규명한 것입니다.

  • Figure 4에 나타난 바와 같이, b/d50 값이 증가함에 따라 평형 세굴 심도는 특정 지점(b/d50 ≈ 330)까지 증가하다가 그 이후로는 점차 감소하는 경향을 보였습니다. 이는 교각 폭에 비해 퇴적물이 매우 고와지면 세굴이 오히려 억제될 수 있음을 시사합니다.
  • 이 결과를 바탕으로, 연구팀은 b/d50 값의 범위에 따라 평형 세굴 심도를 예측할 수 있는 두 개의 새로운 상부 포락선 방정식(upper envelope equations)을 제안했습니다.
    • 4 ≤ b/d50 ≤ 37: ds/b = 0.05 * (b/d50) + 1.11
    • 37 ≤ b/d50 ≤ 1 x 10^4: ds/b = 2 / ((0.027 * (b/d50) - 0.6)^1.4 + 1.3) + 1.8

이 방정식들은 기존 연구 데이터와 비교했을 때, 광폭 교각의 세굴 심도를 과소평가 없이 더 정확하게 예측하는 것으로 나타났습니다(Figure 6).

Practical Implications for R&D and Operations

  • For Hydraulic/Civil Design Engineers: 이 연구는 교량 설계 시 퇴적물의 입경을 중요한 설계 변수로 고려해야 함을 명확히 보여줍니다. 제안된 방정식을 활용하면 특정 하천 조건(퇴적물 크기)에 맞는 광폭 교각의 세굴 심도를 더 정밀하게 예측하여, 과잉 설계를 피하고 경제적인 기초 설계를 수행할 수 있습니다.
  • For Structural Integrity Analysts: 세굴 심도 예측의 정확도 향상은 교량의 장기적인 안정성 평가에 직접적으로 기여합니다. 특히 b/d50 비율이 큰(매우 고운 퇴적물) 환경에서는 세굴이 특정 수준 이상으로 발달하지 않을 수 있다는 점을 고려하여 유지보수 및 보강 계획을 최적화할 수 있습니다.
  • For CFD Simulation Specialists: 본 연구에서 제공된 상세한 물리 모델 실험 데이터(Figure 1의 시간별 세굴 데이터 등)는 CFD 모델의 검증(validation)을 위한 귀중한 자료로 활용될 수 있습니다. 특히 말굽 와류의 거동과 퇴적물 이동을 모사하는 수치 모델의 정확도를 높이는 데 기여할 수 있습니다.

Paper Details


Modelling the Effect of Sediment Coarseness on Local Scour at Wide Bridge Piers

1. Overview:

  • Title: Modelling the Effect of Sediment Coarseness on Local Scour at Wide Bridge Piers
  • Author: Nordila, Ahmad; Thamer, Mohammad; Melville, Bruce W.; Faisal, Ali; Badronnisa, Yusuf
  • Year of publication: 2017
  • Journal/academic society of publication: Pertanika Journal of Science & Technology
  • Keywords: Physical model, scour, wide piers, uniform sediment, sediment coarseness

2. Abstract:

본 논문은 두 종류의 균일한 퇴적물 바닥에 설치된 원통형 광폭 교각 주변의 세굴에 대한 물리적 모델 실험 데이터를 제시한다. 퇴적물 입경과 다양한 교각 폭이 광폭 교각의 세굴 발달 및 평형 세굴 심도에 미치는 영향을 기술한다. 기존 문헌들은 실험실 데이터에 기반한 경험적 세굴 예측 공식이 대형 구조물의 세굴 심도를 과대 예측한다고 제안한다. 본 연구는 원통형 광폭 교각에 대한 이러한 격차를 메우고자 시도했다. 더 나아가, 균일한 퇴적물에 설치된 광폭 원통형 교각의 무차원 최대 세굴 심도를 퇴적물 조도의 함수로 추정하기 위한 방정식들이 제안되었다.

3. Introduction:

많은 연구가 교량 교각의 최대 세굴 심도를 개발하는 것을 목표로 수행되어 왔다. 그러나 광폭 교각의 세굴 심도 측정에 대한 연구는 제한적이다. 광폭 교각은 얕은 수로에 위치하며 유속이 느리고, 프루드 수(Froude number) < 0.8에 대해 y/b < 0.8로 정의된다. 기존 연구들은 b/d50, 즉 퇴적물 조도 매개변수가 광폭 교각의 평형 국부 세굴 심도에 상당한 영향을 미친다는 것을 보여주었다. 문헌의 예측 방정식들은 대형 및 소형 교각 모두를 대상으로 하므로, 이러한 교각에서 국부 세굴을 과대 예측하게 되어 불필요하고 비용이 많이 드는 기초 공사나 대책을 사용하게 만든다. 따라서 본 연구는 두 가지 균일한 퇴적물 크기와 다섯 개의 교각 모델을 사용하여 퇴적물 조도(b/d50)의 효과를 조사하기 위해 실험실에서 국부 교각 세굴 실험을 수행했다.

4. Summary of the study:

Background of the research topic:

교량의 안전성을 위협하는 주요 요인 중 하나는 교각 주변의 국부 세굴 현상이다. 특히 교각 폭이 수심에 비해 상대적으로 넓은 ‘광폭 교각’의 경우, 기존의 세굴 예측 공식이 실제보다 과도한 세굴 깊이를 예측하는 경향이 있어 설계의 비경제성을 초래했다.

Status of previous research:

Johnson & Torrico (1994), Arneson et al. (2012), Sheppard et al. (2004), Lee & Sturm (2009) 등 다수의 연구에서 광폭 교각의 세굴 특성과 퇴적물 크기(b/d50)의 중요성을 지적했다. 그러나 대부분의 공식은 여전히 실제 대형 구조물의 세굴을 과대평가하는 한계를 가지고 있었다.

Purpose of the study:

본 연구의 목적은 광폭 원통형 교각에서 퇴적물 조도(b/d50)가 국부 세굴 발달 및 평형 세굴 심도에 미치는 영향을 실험적으로 규명하고, 이를 바탕으로 더 정확한 세굴 심도 예측 방정식을 개발하는 것이다.

Core study:

두 종류의 퇴적물(d50 = 0.23mm, 0.80mm)과 다섯 가지 직경의 교각 모델을 사용하여 총 10회의 수리 실험을 수행했다. 시간 경과에 따른 세굴 구멍의 발달 과정과 최종 평형 세굴 심도를 측정하고, 이를 무차원 변수인 퇴적물 조도(b/d50)와 상대 세굴 심도(ds/b)의 관계로 분석했다.

5. Research Methodology

Research Design:

대규모 수조(flume)를 이용한 물리적 모델링 실험으로 설계되었다. 교각 직경(b)과 퇴적물 입경(d50)을 주요 변수로 설정하고, 흐름 조건(U/Uc ≈ 0.95)은 일정하게 유지하여 변수의 영향을 명확히 분석하고자 했다.

Data Collection and Analysis Methods:

시간 경과에 따른 세굴 깊이(ds)를 측정하여 세굴 발달 과정을 기록했다. 최종 평형 상태에 도달했을 때의 최대 세굴 심도를 측정하여 데이터를 수집했다. 수집된 데이터는 무차원 변수(ds/b, b/d50)로 변환하여 그래프로 분석하고, 다른 연구자들의 데이터와 비교 분석하여 새로운 예측 방정식을 도출했다.

Research Topics and Scope:

연구는 원통형 광폭 교각, 균일한 무점착성 퇴적물, 그리고 퇴적물 이동이 막 시작되는 한계 유속 조건(clear-water scour)에 국한된다.

6. Key Results:

Key Results:

  • 세굴 발달은 초기, 주 침식, 평형의 3단계로 구분되며, 퇴적물 조도(b/d50)에 따라 침식 양상이 달라진다.
  • 상대 평형 세굴 심도(ds/b)는 퇴적물 조도(b/d50)가 증가함에 따라 감소하는 전반적인 경향을 보인다.
  • b/d50 ≈ 330에서 최대 세굴 심도가 관찰되었으며, 이보다 값이 커지면 세굴 심도는 오히려 감소했다.
  • 퇴적물 조도(b/d50)를 기반으로 평형 세굴 심도를 예측하는 두 개의 연속적인 상부 포락선 방정식을 개발했다.
Figure 3. b = 140 mm, d50 = 0.80 mm, b/d50 = 175, U/Uc = 0.95
Figure 3. b = 140 mm, d50 = 0.80 mm, b/d50 = 175, U/Uc = 0.95

Figure Name List:

  • Figure 1. Normalised local scour depth (ds/b) versus time at the same value of b in sediment beds of d50=0.23 and 0.80 mm
  • Figure 2. b = 140 mm, d50 = 0.23 mm, b/d50 = 609, U/Uc = 0.95
  • Figure 3. b = 140 mm, d50 = 0.80 mm, b/d50 = 175, U/Uc = 0.95
  • Figure 4. Equilibrium scour depth versus b/d50 for the present study
  • Figure 5. Effect of b/d50 on ds/b
  • Figure 6. Comparison of observed values of ds/b around wide piers with those predicted using Equation [1] and Equation [2]

7. Conclusion:

본 연구는 유속 강도 U/Uc = 0.95 조건에서 새로운 실험 데이터를 통해 국부 세굴 심도의 시간적 및 공간적 발달을 보여주었다. 광폭 교각에서의 국부 세굴 심도가 세굴 구멍 발달 및 퇴적물 조도에 미치는 영향이 제시되었다. 상대 세굴 심도(dse/b)는 퇴적물 조도 값이 증가함에 따라 감소하는 것으로 나타났다. b/d50 값에 따라 교각 세굴 심도를 예측하는 두 개의 연속적인 상부 포락선 방정식이 개발되었다. b/d50 값이 클 때 dse/b 값이 감소하는 것이 입증되었으며, 이는 대형 수조를 사용한 실험 결과 및 이전 연구자들의 발견과 일치했다.

8. References:

  • Arneson, L. A., Zevenbergen, L. W., Lagasse, P. F., & Clopper, P. E. (2012). Evaluating scour at bridges (4th Ed.). Hydraulic Engineering Circular No. 18 (HEC-18). Federal Highway Administration, Washington, DC.
  • Ettema, R., (1980). Scour around bridge piers. Report No. 216, University of Auckland, Auckland, New Zealand.
  • Ettema, R., Kirkil, G., & Muste, M. (2006). Similitude of large-scale turbulence in experiments on local scour at cylinders. Journal of Hydraulic Engineering, 132(1), 33-40.
  • Johnson, P. A., & Torrico, E. F. (1994). Scour around wide piers in shallow water. Transportation Research Record, (1471), 66-70.
  • Johnson, P. A. (1999). Scour at Wide Piers Relative to Flow Depth, Stream Stability and Scour at Highway Bridges. In E. V. Richardson & P. F. Lagasse (Eds.), Compendium of ASCE Conference Papers (pp. 280–287).
  • Jones, J., & Sheppard, D. (2000). Scour at wide bridge pier (pp. 1-10). Federal Highway Administration, Turner-Fairbank Highway Research Center, McLean, Virginia.
  • Junliang, T., & Xiong, Y. (2014). Flow and Scour Patterns around Bridge Piers with Different Configurations: Insights from CFD Simulations. In Geo-Congress 2014 Technical Papers: Geo-characterization and Modeling for Sustainability (pp. 2655-2664). ASCE.
  • Kirkil, G., Constantinescu, S. G., & Ettema, R., (2008). Coherent structures in the flow field around a circular cylinder with scour hole. Journal of Hydraulic Engineering, 134(5), 572–587.
  • Lança, R. M., Fael, C. S., Maia, R. J., Pêgo, J. P., & Cardoso, A. H. (2013). Clear-water scour at comparatively large cylindrical piers. Journal of Hydraulic Engineering, 139(11), 1117-1125.
  • Lee, S. O., & Sturm, T. W. (2009). Effect of sediment size scaling on physical modeling of bridge pier scour. Journal of Hydraulic Engineering, 135(10), 793-802.
  • Melville, B. W., & Coleman, S. E., (2000). Bridge Scour. United States of America, USA: Water Resources Publications.
  • Melville, B.W., (1975). Local scour at bridge sites. Report No.117. School of Engineering, University of Auckland, New Zealand.
  • Melville, B. W. (2008). The physics of Local Scour at Bridge Piers. In Fourth International Conference on Scour and Erosion (pp. 28-38). Tokyo.
  • Nicolet, G. (1971). Deformation des lits alluvionaires affouillements autor des piles se ponts cylindriques. Report No. HC 043 684. Laboratoire National d’Hydraulique, Chatou, France.
  • Sheppard, D. M., Huseyin, D., & Melville, B. W. (2011). Scour at wide piers and long skewed piers. Report (National Cooperative Highway Research Program); 682. Washington, D.C.: Transportation Research Board.
  • Sheppard, D. M., Melville, B., & Demir, H. (2013). Evaluation of existing equations for local scour at bridge piers. Journal of Hydraulic Engineering, 140(1), 14-23.
  • Sheppard, D. M., & Miller, J. W. (2006). Live-bed local pier scour experiments. Journal of Hydraulic Engineering, 132(7), 635-642.
  • Sheppard, D. M., Odeh, M., & Glasser, T. (2004). Large scale clear-water local pier scour experiments. Journal of Hydraulic Engineering, 130(10), 957-963.

Expert Q&A: Your Top Questions Answered

Q1: 실험에서 흐름 강도(U/Uc)를 0.95로 설정한 특별한 이유가 있나요?

A1: 흐름 강도를 0.95로 설정한 것은 ‘清水 세굴(clear-water scour)’ 조건, 즉 상류로부터 유입되는 퇴적물 없이 순수하게 교각 주변의 흐름 변화만으로 세굴이 발생하는 조건을 모사하기 위함입니다. 이 값은 퇴적물 입자가 움직이기 시작하는 한계점에 매우 가까운 상태로, 교각으로 인한 국부적인 유속 증가 및 와류 효과를 가장 극명하게 관찰할 수 있는 최적의 조건입니다. 실제 교량 환경에서도 홍수 초기 단계 등에서 유사한 조건이 발생할 수 있습니다.

Q2: 퇴적물 조도(b/d50)가 특정 값(약 330)을 넘어서자 세굴 심도가 오히려 감소하는 이유는 무엇인가요? (Figure 4 참조)

A2: 이는 교각 폭(b)에 비해 퇴적물 입자(d50)가 매우 작아지는 경우에 발생하는 현상입니다. 논문에 따르면, b/d50 값이 매우 크다는 것은 상대적으로 고운 퇴적물을 의미합니다. 이 경우, 교각 주변에서 발생하는 하강류와 말굽 와류의 에너지가 세굴 구멍을 깊게 파는 데 효과적으로 작용합니다. 하지만 일정 수준을 넘어서면, 세굴 구멍의 경사면 안정성이나 와류 구조의 변화 등 다른 물리적 메커니즘이 작용하여 세굴 심도의 증가를 억제하는 것으로 해석됩니다. 이는 더 큰 교각에서 국부적인 상류부 침식이 세굴 발달에 영향을 미치는 것과도 관련이 있습니다.

Q3: 본 연구에서 제안된 두 개의 예측 방정식이 b/d50 = 37을 기준으로 나뉘는 이유는 무엇인가요?

A3: Figure 5에 제시된 기존 연구 데이터들을 포함한 전체 데이터 분포를 보면, b/d50 = 37 근방에서 데이터의 경향성이 변하는 것을 관찰할 수 있습니다. 이는 퇴적물이 교각 폭에 비해 상대적으로 ‘거친(coarse)’ 영역에서 ‘중간(intermediate)’ 영역으로 넘어가는 물리적 특성의 변화를 반영하는 것으로 보입니다. 따라서 연구진은 전체 데이터의 경향을 가장 잘 대표할 수 있는 두 개의 연속적인 함수로 모델을 나누어 예측의 정확도를 높였습니다.

Q4: 이 연구 결과는 원통형 교각에만 적용되나요? 사각형이나 다른 형태의 교각에도 적용할 수 있을까요?

A4: 본 연구는 명시적으로 ‘원통형(cylindrical)’ 교각 모델을 사용하여 수행되었으므로, 제안된 방정식들은 원통형 교각에 가장 적합합니다. 교각의 형태는 주변 흐름 구조, 특히 말굽 와류와 후류(wake)의 특성을 크게 변화시키므로 사각형이나 유선형 교각에는 다른 보정 계수가 필요하거나 별도의 연구가 요구됩니다. 하지만 퇴적물 조도(b/d50)가 세굴에 중요한 영향을 미친다는 근본적인 물리 현상은 다른 형태의 교각에서도 유사하게 나타날 것으로 예상할 수 있습니다.

Q5: 이 연구는 실험실 규모의 실험인데, 실제 대규모 하천에 직접 적용할 때 주의할 점은 무엇인가요?

A5: 본 연구는 대규모 수조를 사용했지만, 실제 하천의 복잡성에 비하면 여전히 통제된 환경입니다. 실제 하천에 적용할 때는 불규칙한 하상 형태, 식생의 영향, 흐름의 비정상성(unsteadiness), 그리고 불균일한 퇴적물 분포 등 축척 효과(scale effects)와 현장의 복잡성을 고려해야 합니다. 따라서 제안된 방정식은 예비 설계나 기본 분석 단계에서 유용한 도구가 될 수 있으며, 최종 설계에서는 현장 데이터나 정밀한 3차원 수치 모델링(CFD)을 통한 검증이 병행되는 것이 바람직합니다.


Conclusion: Paving the Way for Higher Quality and Productivity

기존 예측 모델의 한계로 인해 발생했던 광폭 교량 교각 세굴 심도의 과대평가 문제는 교량 설계의 경제성과 효율성을 저해하는 요인이었습니다. 본 연구는 퇴적물 조도(b/d50)라는 핵심 물리적 변수를 통해 이 문제에 대한 명확한 해답을 제시했습니다. 실험을 통해 퇴적물 조도가 증가할수록 상대적 세굴 심도가 감소하는 경향을 정량적으로 입증하고, 이를 기반으로 한 새로운 예측 방정식을 개발함으로써 교량 설계의 정확도를 한 단계 끌어올렸습니다.

이러한 연구 결과는 더 안전하고 경제적인 교량 인프라 구축에 직접적으로 기여하며, 토목 수리 공학 분야의 기술 발전을 이끄는 중요한 이정표가 될 것입니다.

(주)에스티아이씨앤디에서는 고객이 수치해석을 직접 수행하고 싶지만 경험이 없거나, 시간이 없어서 용역을 통해 수치해석 결과를 얻고자 하는 경우 전문 엔지니어를 통해 CFD consulting services를 제공합니다. 귀하께서 당면하고 있는 연구프로젝트를 최소의 비용으로, 최적의 해결방안을 찾을 수 있도록 지원합니다.

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Copyright Information

  • This content is a summary and analysis based on the paper “Modelling the Effect of Sediment Coarseness on Local Scour at Wide Bridge Piers” by “Nordila, Ahmad et al.”.
  • Source: https://core.ac.uk/display/85259972

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Gambar 1. Ilustrasi gerusan lokal di sekitar pilar jembatan (Sumber : Coastal Engineering Research Center dalam cahyono dan solichin, 2008)

실험 데이터로 검증: 교각 보호 장치 각도가 국부 세굴에 미치는 영향 분석

이 기술 요약은 Sarbaini, Mudjiatko, Rinaldi가 Jom FTEKNIK (2015)에 발표한 논문 “MODEL LABORATORIUM PENGARUH VARIASI SUDUT ARAH PENGAMAN PILAR TERHADAP KEDALAMAN GERUSAN LOKAL PADA JEMBATAN DENGAN PILAR CYLINDER GROUPED”를 바탕으로, STI C&D의 기술 전문가에 의해 분석 및 요약되었습니다.

Keywords

  • Primary Keyword: 교각 세굴 (Bridge Pier Scour)
  • Secondary Keywords: 국부 세굴 (Local Scour), CFD 시뮬레이션 (CFD Simulation), 교량 안전 (Bridge Safety), 수리 동역학 (Hydrodynamics), 퇴적물 이동 (Sediment Transport)

Executive Summary

  • The Challenge: 만곡 하천에 설치된 교량의 교각은 국부 세굴 현상으로 인해 기초가 약화되어 구조적 안정성에 심각한 위협을 받습니다.
  • The Method: 실험실 수로 모델을 사용하여 그룹 원통형 교각 주변에 커튼형 보호 장치를 59°, 50°, 90°의 세 가지 각도로 설치하고, 각 조건에서 발생하는 세굴 깊이를 측정했습니다.
  • The Key Breakthrough: 교각 보호 장치의 설치 각도가 세굴 깊이에 결정적인 영향을 미치며, 특정 조건에서 보호 장치의 세굴 깊이 비율(ds/b)이 최대 2.4에 도달하는 것을 확인했습니다.
  • The Bottom Line: 교량의 장기적인 내구성을 확보하기 위해서는 세굴 보호 장치의 각도를 최적화하는 것이 매우 중요하며, 본 실험 데이터는 예측 CFD 모델의 정확성을 검증하는 핵심적인 기준을 제공합니다.

The Challenge: Why This Research Matters for CFD Professionals

하천에 건설된 교량, 특히 유속이 빠르고 흐름이 복잡한 만곡부에 위치한 교량의 교각은 지속적인 수리동역학적 힘과 나선형 흐름(helicoidal flow)에 노출됩니다. 이러한 힘은 교각 주변의 하상 재료를 침식시키는 국부 세굴(local scouring) 현상을 유발합니다. 세굴이 심화될 경우 교각의 기초가 노출되고 지지력이 약화되어 최악의 경우 교량 붕괴로 이어질 수 있습니다. 따라서 교각의 안정성을 확보하기 위해 다양한 형태의 보호 장치가 사용되지만, 그 효과를 극대화하기 위한 최적의 설계 기준은 여전히 중요한 연구 과제입니다. 본 연구는 보호 장치의 ‘설치 각도’라는 특정 변수가 세굴 깊이에 미치는 영향을 정량적으로 분석하여, 보다 안전하고 경제적인 교량 설계의 기초를 마련하고자 했습니다.

The Approach: Unpacking the Methodology

본 연구는 실제 하천의 복잡한 현상을 통제된 환경에서 재현하기 위해 실험실 모델을 사용했습니다. 연구의 핵심적인 방법론은 다음과 같습니다.

  • 실험 장비: 재순환 퇴적물 수로(Recirculating sediment flume)를 사용하여 연속적인 흐름 조건을 구현했습니다. 수로의 크기는 길이 8m, 폭 0.8m, 높이 0.15m입니다.
  • 교각 모델: 실제 Teratak Buluh 교량의 형태를 채택한 그룹 원통형(grouped cylinder) 교각 모델을 사용했습니다. 이는 2개의 그룹으로 구성되며, 그룹 1은 12개, 그룹 2는 10개의 기둥으로 이루어져 있습니다.
  • 하상 재료: 캄파르(Kampar) 강 모래를 사용했으며, 입자 크기 분포는 d35 = 0.247mm, d50 = 0.298mm, d65 = 0.352mm, 비중(Gs)은 2.64입니다.
  • 핵심 변수: 교각 보호 장치(curtain type)의 설치 각도를 59°(θ1), 50°(θ2), 90°(θ3) 세 가지로 변화시켰습니다. 또한, 프루드 수(Froude number) 0.464에서 0.698 범위의 세 가지 아임계 흐름(subcritic flow) 조건을 적용하여 유속의 영향을 함께 평가했습니다. 레이놀즈 수(Reynolds number) 계산 결과, 흐름은 천이류(transition flow)와 난류(turbulence flow) 영역에 해당했습니다.
Gambar 1. Ilustrasi gerusan lokal di sekitar pilar jembatan (Sumber : Coastal Engineering Research Center dalam cahyono dan solichin, 2008)
Gambar 1. Ilustrasi gerusan lokal di sekitar pilar jembatan (Sumber : Coastal Engineering Research Center dalam cahyono dan solichin, 2008)

The Breakthrough: Key Findings & Data

실험을 통해 교각 보호 장치의 각도와 유속이 세굴 깊이에 미치는 영향을 정량적으로 분석했으며, 주요 결과는 다음과 같습니다.

Gambar 4. Ilustrasi 3D model pilar dan pengaman pilar jembatan (a) group pile 1, (b) group pile 2.
Gambar 4. Ilustrasi 3D model pilar dan pengaman pilar jembatan (a) group pile 1, (b) group pile 2.

Finding 1: 보호 장치 각도와 세굴 깊이의 직접적인 상관관계

보호 장치의 각도는 교각과 보호 장치 자체의 세굴 깊이에 직접적인 영향을 미쳤습니다. 결론(G.2)에 따르면, 교각 그룹 1의 경우, 90° 각도에서 가장 큰 세굴(ds/b = 1.5)이 발생했으며, 59° 각도에서 가장 작은 세굴(ds/b = 1.3)이 나타났습니다. 특히 주목할 점은 보호 장치 자체의 세굴입니다. 90° 각도에서 보호 장치의 세굴 깊이 비율은 2.4로 가장 컸고, 50° 각도에서는 1.5로 가장 작았습니다. 이는 보호 장치의 각도가 흐름을 교란시키는 방식에 따라 침식 에너지가 집중되는 위치와 강도가 달라짐을 명확히 보여줍니다.

Finding 2: 유동 조건과 퇴적물 이동의 연관성

더 높은 프루드 수(Froude number)를 가진 흐름, 즉 유속이 빠를수록 더 큰 입경의 퇴적물이 이동하는 것으로 확인되었습니다(결론 G.3). 쉴드(Shields) 및 휼스트롬(Hjulstorm) 다이어그램 분석 결과(그림 8, 9, 10), 실험에 사용된 모든 입자 등급은 ‘이동 영역(moving zone)’에 위치했습니다. 이는 실험 조건이 하상 재료가 지속적으로 이동하는 ‘이동상 세굴(live-bed scour)’ 환경이었음을 의미하며, 실제 홍수 시 발생하는 현상과 유사합니다. 이 결과는 유속이 세굴의 직접적인 원동력이며, 흐름의 에너지가 침식 능력과 직결됨을 입증합니다.

Practical Implications for R&D and Operations

  • For Process Engineers (토목/수리 엔지니어): 본 연구는 커튼형 보호 장치의 각도가 신중하게 선택되어야 함을 시사합니다. 시공이 용이해 보이는 90° 각도가 오히려 더 큰 세굴을 유발할 수 있습니다. 이 데이터는 세굴 방지 대책을 위한 설계 가이드라인을 수립하는 데 중요한 정보를 제공합니다.
  • For Quality Control Teams (인프라 검사팀): 논문의 다양한 그래프(그림 13-21)는 유속과 보호 장치 각도에 따라 세굴 패턴이 어떻게 다르게 발달하는지 보여줍니다. 이는 교량 정기 점검 시, 본 실험에서 고위험 지역으로 식별된 구역을 집중적으로 확인할 수 있는 검사 프로토콜을 개발하는 데 활용될 수 있습니다.
  • For Design Engineers (교량 설계자): 연구 결과는 교각과 보호 시스템의 기하학적 구성이 세굴을 제어하는 핵심 변수임을 나타냅니다. 이 연구는 단순한 교각 형상 설계를 넘어, 보호 장치의 역할과 최적 배치에 대한 정량적 데이터를 제공함으로써 초기 설계 단계에서 중요한 고려사항을 제시합니다.

Paper Details


MODEL LABORATORIUM PENGARUH VARIASI SUDUT ARAH PENGAMAN PILAR TERHADAP KEDALAMAN GERUSAN LOKAL PADA JEMBATAN DENGAN PILAR CYLINDER GROUPED

1. Overview:

  • Title: MODEL LABORATORIUM PENGARUH VARIASI SUDUT ARAH PENGAMAN PILAR TERHADAP KEDALAMAN GERUSAN LOKAL PADA JEMBATAN DENGAN PILAR CYLINDER GROUPED
  • Author: Sarbaini, Mudjiatko, Rinaldi
  • Year of publication: 2015
  • Journal/academic society of publication: Jom FTEKNIK Volume 2 No. 2 Oktober 2015
  • Keywords: local scouring, grouped cylinder pillar, angle of pillars protector, curtain type pillars protectot, depth ratio

2. Abstract:

Bridge pillars placed on meander river experience hydrodynamic flow and helecoidal force. Those force will cause local scour on pillars and pillar protectors. Pillar protectors with specified angle is expected to be able to minimize the magnitude of scouring on pillars. Laboratory model with grouped cylinder type pillars with three variation of angle of curtain type pillars protector (θ1, θ2, θ3) are used to observed the phenomenon of scouring that occured on meander river. Kampar sand with grain size of d35 = 0,247 mm, d50 = 0,298 mm, d65 = 0,352 mm and Gs = 2,64 are used as the base for the bed of the channel. Three type of subcritic flow with froude number ranged from 0,464-0,698 and yield the reynolds number occured on Fr1-Fr3 at 1658,416 thus classified as transition flow while 3081,683 and 4381,188 are classified as turbulence flow. Shield graphic showed that grain gradation used in this research is located one moving zone. The ratio of scouring depth (ds/b) of pillars protectors is highest 2,4 that occured on Fr3 θ2 and Fr1 θ3 while on the pillars is occured on Fr2 θ2 at 1,9. The results of sediment transport analysis proved that with the in crease in froude number used the bigger the size of the grain transported.

3. Introduction:

만곡 형태의 하천(meander)은 일반적으로 완만한 하상 경사를 가집니다. 만곡부 외측은 내측보다 유속이 빠르기 때문에 하상이 더 깊어지는 경향이 있으며, 원심력으로 인해 횡방향 흐름이 발생하고 주 흐름과 결합하여 나선형 흐름(helicoidal flow)을 형성합니다. 하천의 흐름은 종종 퇴적물 이동과 세굴 과정을 동반합니다. 세굴은 하천의 형태학적 영향이나 흐름을 방해하는 구조물로 인해 자연적으로 발생할 수 있습니다. 이러한 흐름 속에 위치한 교량 교각은 3차원 흐름과 흐름 패턴의 변화를 유발하여 구조물 주변에 국부적인 세굴을 일으킵니다.

4. Summary of the study:

Background of the research topic:

만곡 하천에 설치된 교량 교각은 복잡한 수리동역학적 힘에 의해 국부 세굴에 취약합니다. 이는 교량의 구조적 안정성을 위협하므로, 세굴을 최소화하기 위한 효과적인 교각 보호 장치 설계가 필요합니다.

Status of previous research:

과거 Arie Perdana Putra (2014)는 그룹 원통형 교각의 국부 세굴에 대한 실험실 모델 연구를 수행했으며, Tri Achmadi (2001)는 교각 세굴에 대한 수리 모델 연구를 진행한 바 있습니다.

Purpose of the study:

본 연구의 목적은 만곡 하천에 설치된 그룹 원통형 교각에서, 커튼형 보호 장치의 설치 각도(59°, 50°, 90°)를 변화시켰을 때 세굴 현상이 어떻게 달라지는지 규명하는 것입니다.

Core study:

실험실 수로에서 그룹 원통형 교각 모델과 세 가지 다른 각도의 보호 장치를 사용하여 국부 세굴 깊이를 측정하고, 프루드 수에 따른 흐름 조건의 변화가 세굴 및 퇴적물 이동에 미치는 영향을 분석했습니다.

5. Research Methodology

Research Design:

통제된 실험실 환경에서 교각 보호 장치의 각도라는 독립 변수가 국부 세굴 깊이라는 종속 변수에 미치는 영향을 측정하는 실험 연구 설계를 채택했습니다.

Data Collection and Analysis Methods:

수로 내에 교각 및 보호 장치 모델을 설치하고, 특정 유속(프루드 수 기준) 조건에서 일정 시간 동안 흐름을 발생시킨 후, 교각 주변의 하상 변화(세굴 깊이)를 측정했습니다. 또한, 실험 전후의 하상 재료 입도 분석을 통해 퇴적물 이동 특성을 분석했습니다.

Research Topics and Scope:

연구는 그룹 원통형 교각, 커튼형 보호 장치, 그리고 세 가지 특정 설치 각도(59°, 50°, 90°)에 국한됩니다. 흐름 조건은 세 가지 아임계 흐름으로 제한되었으며, 하상 재료는 캄파르 강 모래를 사용했습니다.

6. Key Results:

Key Results:

  • 레이놀즈 수에 근거하여, Fr1 흐름은 천이류(Re = 1658.416)로, Fr2 및 Fr3 흐름은 난류(Re > 2000)로 분류되었습니다.
  • 교각 그룹 1에 대한 Fr1 시험에서, 세굴 깊이 비율(ds/b)은 59° 각도에서 1.3으로 가장 작았고, 90° 각도에서 1.5로 가장 컸습니다.
  • 교각 그룹 1의 보호 장치에서는 50° 각도에서 세굴이 1.5(ds/b)로 가장 작았고, 90° 각도에서 2.4로 가장 컸습니다.
  • 교각 그룹 2에서는 59°와 50° 각도에서 세굴이 1.3(ds/b)으로 가장 작았고, 90° 각도에서 1.4로 가장 컸습니다.
  • 교각 그룹 2의 보호 장치에서는 50° 각도에서 세굴이 1.7(ds/b)로 가장 컸고, 90° 각도에서 1.4로 가장 작았습니다.
  • 프루드 수가 증가할수록 더 큰 입경의 퇴적물이 이동하는 것으로 분석되었습니다.

Figure List:

  • Gambar 1. Ilustrasi gerusan lokal di sekitar pilar jembatan
  • Gambar 2. Metode pengendalian gerusan
  • Gambar 3. Recirculating sediment flume
  • Gambar 4. Ilustrasi 3D model pilar dan pengaman pilar jembatan (a) group pile 1, (b) group pile 2.
  • Gambar 5. Sudut Pengaman Pilar
  • Gambar 6. Bagan alir penelitian
  • Gambar 7. Distribusi kecepatan permukaan Fr1
  • Gambar 8. Grafik gerak awal butiran Shields
  • Gambar 9. Grafik Shields modifikasi Breusers dan Raudkivi
  • Gambar 10. Grafik gerak awal butiran Hjulstorm
  • Gambar 11. Ilustrasi pola aliran pada model pilar jembatan
  • Gambar 12. Posisi profil memanjang dan melintang pada pilar jembatan
  • Gambar 13. Potongan memanjang Sisi Dalam, Sisi Tengah dan Sisi Luar pada Fr1 θ1
  • Gambar 14. Potongan memanjang Sisi Dalam, Sisi Tengah dan Sisi Luar pada Fr2 θ1
  • Gambar 15. Potongan memanjang Sisi Dalam, Sisi Tengah dan Sisi Luar pada Fr3 θ1
  • Gambar 16. Potongan memanjang Sisi Dalam, Sisi Tengah dan Sisi Luar pada Fr₁ θ2
  • Gambar 17. Potongan memanjang Sisi Dalam, Sisi Tengah dan Sisi Luar pada Fr2 θ2
  • Gambar 18. Potongan memanjang Sisi Dalam, Sisi Tengah dan Sisi Luar pada Fr3 θ2
  • Gambar 19. Potongan memanjang Sisi Dalam, Sisi Tengah dan Sisi Luar pada Fr1 θ3
  • Gambar 20. Potongan memanjang Sisi Dalam, Sisi Tengah dan Sisi Luar pada Fr2 θ3
  • Gambar 21. Potongan memanjang Sisi Dalam, Sisi Tengah dan Sisi Luar pada Fr3 θ3
  • Gambar 22. Potongan memanjang C-C pada θ1
  • Gambar 23. Potongan memanjang H-H pada θ1
  • Gambar 24. Potongan memanjang C-C pada θ2
  • Gambar 25. Potongan memanjang H-H pada θ2
  • Gambar 26. Potongan memanjang C-C pada θ3
  • Gambar 27. Potongan memanjang H-H pada θ3
  • Gambar 28. Potongan melintang J-J
  • Gambar 29. Potongan melintang M-M
  • Gambar 30. Potongan melintang N-N
  • Gambar 31. Perkembangan rasio kedalaman (d/b) terhadap fungsi waktu (t)
  • Gambar 32. Hubungan d 50/d50 terhadap bilangan Froude

7. Conclusion:

실험실 모델을 통한 연구 결과, 교각 보호 장치의 각도와 흐름 조건은 국부 세굴 깊이에 상당한 영향을 미치는 것으로 나타났습니다. 레이놀즈 수 분석을 통해 흐름이 천이류 및 난류 영역에 있음을 확인했습니다. 세굴 깊이 비율(ds/b)은 보호 장치의 각도에 따라 민감하게 변화했으며, 특정 조건에서 최대 2.4에 도달했습니다. 또한, 프루드 수가 증가함에 따라 더 큰 퇴적물이 운반되는 현상을 통해 유속과 침식 에너지의 직접적인 관계를 입증했습니다. 이 결과들은 교량의 안전성 확보를 위해 세굴 보호 장치의 기하학적 설계가 매우 중요함을 강조합니다.

8. References:

  • Achmadi, Tri. 2001. Model Hidraulik Gerusan Pada Pilar Jembatan. Tesis. Semarang: Universitas Diponegoro.
  • Alabi, P.D. 2006. Time Development of Local Scour at A Bridge Pier Fitted With A Collar. Tesis. Canada: University of Saskatchewan.
  • Arie, P.P. 2014. Model Laboratorium Gerusan Lokal Pada Pilar Jembatan Tipe Grouped Cylinder. Skripsi. Pekanbaru : Universitas Riau.
  • Breusers, H.N.C. and Raudkivi, A.J. 1991. Scouring. IAHR Hydraulic Structure Design Manual. Rotterdam: A.A. Belkema.
  • Ikhsan, C dan Solichin. 2008. Analisis Susunan Tirai Optimal Sebagai Proteksi Pada Pilar Jembatan Dari Gerusan Lokal. Media Teknik Sipil/Juli 2008 : 85–90.
  • Istiarto. 2012. Materi Kuliah Transport Sedimen. Yogyakarta: UGM.
  • Laursen, E.M. and Toch A. 1956. Scour Around Bridge Piers and Abutments. Iowa Highway Research Board Bulletin No. 4 :1-60.
  • Legono, 1988, Diktat Teknik Sungai, UGM, Yogyakarta.
  • Melville, B.W. 1975. Local Scour at Bridge Sites. Tesis. New Zealand: University of Auckland.
  • Mudjiatko. 2000. Pengaruh Meander Sungai Terhadap Perubahan Konfigurasi Dasar dan Seleksi Butiran Sedimen. Yogyakarta.
  • Nichols, Gary. 2009. Sedimentology and Stratigraphy. United Kingdom: Wiley-Blackwell.
  • Rinaldi dan Yulistiyanto, B. 2001. Model Fisik Pengendalian Gerusan Di Sekitar Abutmen Jembatan. Forum Teknik Sipil No. X/2-Agustus 2001 : 139–149.
  • Triatmodjo, B. 1996. Hidraulika II. Yogyakarta: Beta Offset.
  • Wibowo, O.M. 2007. Pengaruh Aliran Terhadap Gerusan Lokal Di Sekitar Pilar Jembatan. Skripsi. Semarang : Universitas Negeri Semarang.

Expert Q&A: Your Top Questions Answered

Q1: 교각 보호 장치 실험에 59°, 50°, 90°라는 특정 각도를 선택한 이유가 무엇인가요?

A1: 논문에서는 이 세 가지 각도(θ1=59°, θ2=50°, θ3=90°)를 변수로 사용하여 실험을 수행했다고 명시하고 있으나, 이 특정 값들을 선택한 이론적 배경이나 이유는 구체적으로 설명하지 않았습니다. 이 연구는 주어진 각도 변화에 따른 세굴 현상을 관찰하고 정량화하는 데 초점을 맞춘 것으로 보입니다.

Q2: 연구에서 천이류와 난류 흐름이 모두 관찰되었는데, 이러한 흐름 특성의 차이가 세굴 결과에 어떤 영향을 미쳤나요?

A2: 연구 결과는 프루드 수(Fr1, Fr2, Fr3)에 따라 제시되었으며, 이는 각기 다른 흐름(천이류, 난류)에 해당합니다. 전반적으로 프루드 수가 높은 난류 조건(Fr2, Fr3)에서 세굴 깊이가 더 깊어지는 경향이 나타났습니다. 예를 들어, θ1 각도 조건에서 프루드 수가 증가함에 따라 만곡부 중앙과 내측의 세굴이 심화되는 것을 그림 13, 14, 15에서 확인할 수 있습니다. 이는 흐름의 에너지가 클수록 침식 능력이 강해진다는 것을 의미합니다.

Q3: 이 실험에서 ‘그룹 원통형’ 교각 타입을 사용한 것의 중요성은 무엇인가요?

A3: 본 연구에서 사용된 그룹 원통형 교각 모델은 실제 ‘Teratak Buluh’ 교량의 형태를 채택한 것입니다. 이는 실험 결과가 특정 실제 구조물과 직접적인 연관성을 갖도록 하여 연구의 실용성을 높입니다. 또한, 본문(C. Hubungan Pola Aliran Terhadap Pola Gerusan)에서는 그룹 교각의 경우 단일 교각에 비해 후류 와류(wake vortices)가 작게 형성되어 세굴 패턴에 영향을 미친다고 언급하고 있어, 교각의 형태가 세굴 메커니즘을 이해하는 데 중요한 요소임을 보여줍니다.

Q4: 쉴드(Shields) 및 휼스트롬(Hjulstorm) 다이어그램 분석 결과, 모든 퇴적물이 ‘이동 영역’에 있었다는 것은 무엇을 의미하나요?

A4: 이는 실험이 진행되는 동안 하상 재료가 흐름에 의해 지속적으로 움직이는 ‘이동상 세굴(live-bed scour)’ 조건에서 수행되었음을 의미합니다. 이는 하상 재료가 움직이지 않는 한계 유속 이하에서 발생하는 ‘정지상 세굴(clear-water scour)’과 구분되는 중요한 조건입니다. 이동상 세굴은 실제 하천의 홍수 시 발생하는 현상과 더 유사하며, 퇴적물의 유입과 유출이 동시에 일어나므로 더 복잡한 세굴 과정을 나타냅니다.

Q5: 만곡부의 내측, 중앙, 외측에서 세굴 패턴이 다르게 나타나는 이유는 무엇인가요?

A5: 서론에서 설명하듯이, 만곡 하천에서는 원심력의 영향으로 외측의 유속이 내측보다 빠릅니다. 이로 인해 외측 하상이 더 깊어지는 경향이 있습니다. 또한, 주 흐름과 함께 2차 흐름인 나선형 흐름(helicoidal flow)이 발생하여 바닥의 퇴적물을 내측으로 이동시키는 복잡한 흐름 구조가 형성됩니다. 이러한 복합적인 흐름 특성 때문에 만곡부의 위치에 따라 세굴과 퇴적이 다르게 나타나는 것입니다.


Conclusion: Paving the Way for Higher Quality and Productivity

본 연구는 교각 보호 장치의 설치 각도가 교각 세굴을 제어하는 데 얼마나 중요한 설계 변수인지를 실험 데이터를 통해 명확하게 보여주었습니다. 90°와 같은 단순한 각도가 오히려 더 큰 세굴을 유발할 수 있다는 사실은, 세심한 수리동역학적 분석 없이는 최적의 설계를 달성하기 어렵다는 점을 시사합니다.

이러한 물리적 실험은 CFD 시뮬레이션 모델의 정확성을 검증하는 데 필수적인 데이터를 제공합니다. CFD 해석을 활용하면 본 연구에서 다룬 세 가지 각도 외에도 훨씬 더 광범위한 각도, 유속, 교각 형상 조합을 빠르고 비용 효율적으로 탐색하여 진정한 최적의 설계안을 도출할 수 있습니다.

(주)에스티아이씨앤디에서는 고객이 수치해석을 직접 수행하고 싶지만 경험이 없거나, 시간이 없어서 용역을 통해 수치해석 결과를 얻고자 하는 경우 전문 엔지니어를 통해 CFD consulting services를 제공합니다. 귀하께서 당면하고 있는 연구프로젝트를 최소의 비용으로, 최적의 해결방안을 찾을 수 있도록 지원합니다.

  • 연락처 : 02-2026-0442
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Copyright Information

  • This content is a summary and analysis based on the paper “MODEL LABORATORIUM PENGARUH VARIASI SUDUT ARAH PENGAMAN PILAR TERHADAP KEDALAMAN GERUSAN LOKAL PADA JEMBATAN DENGAN PILAR CYLINDER GROUPED” by “Sarbaini, Mudjiatko, Rinaldi”.
  • Source: Jom FTEKNIK Volume 2 No. 2 Oktober 2015

This material is for informational purposes only. Unauthorized commercial use is prohibited. Copyright © 2025 STI C&D. All rights reserved.

Figure 13 | 3D illustration of Fr variation in the old stilling basin at (a) 129.10 m tailwater, (b) 129.70 m tailwater, and (c) 130.30 m tailwater. In the new stilling basin at (d) 129.10 m tailwater, (e) 129.70 m tailwater, and (f) 130.30 m tailwater

Hydraulic investigation of stilling basins of the barrage before and after remodelling using FLOW-3D

Figure 13 | 3D illustration of Fr variation in the old stilling basin at (a) 129.10 m tailwater, (b) 129.70 m tailwater, and (c) 130.30 m tailwater.
In the new stilling basin at (d) 129.10 m tailwater, (e) 129.70 m tailwater, and (f) 130.30 m tailwater
Figure 13 | 3D illustration of Fr variation in the old stilling basin at (a) 129.10 m tailwater, (b) 129.70 m tailwater, and (c) 130.30 m tailwater. In the new stilling basin at (d) 129.10 m tailwater, (e) 129.70 m tailwater, and (f) 130.30 m tailwater

이 소개자료는 “2023, Water Supply”에서 발표된 “Hydraulic investigation of stilling basins of the barrage before and after remodelling using FLOW-3D” 논문에 대한 소개자료입니다.

연구 목적

  • 본 연구는 FLOW-3D를 사용하여 보의 감세지의 개조 전후 수리학적 성능을 조사하는 것을 목적으로 함.

연구 방법:

모델링 설정

  • FLOW-3D 소프트웨어를 사용하여 개조 전후의 감세지에서 자유 표면, 수심, 프루드 수, 롤러 길이, 유속, 도수 효율, 난류 운동 에너지와 같은 수리학적 매개변수를 시뮬레이션하고 비교 분석하였음.
  • 개조 전 감세지에는 방해벽과 마찰 블록이 있었고, 개조 후에는 슈트 블록과 톱니 모양의 여울로 대체되었음.
  • 문헌 결과와의 비교를 통해 모델의 정확성을 검증하였음.

모델 검증

  • FLOW-3D 모델을 사용하여 개조 전후 감세지의 수리학적 특성을 분석하고, 문헌 결과와 비교하였음.
  • 감세지에서 발생하는 도수 현상의 특성을 파악하고, 개조가 도수에 미치는 영향을 평가하였음.
  • 다양한 수리학적 매개변수를 비교 분석하여 모델의 신뢰성을 검증하였음.

주요 결과:

흐름 특성 분석

  • 개조 전후 감세지에서의 자유 표면, 수심, 유속 분포 등을 FLOW-3D 모델을 통해 분석하였음.
  • 도수 현상의 길이, 높이, 에너지 손실 등을 비교 분석하여 개조의 영향을 평가하였음.
  • 난류 강도 및 롤러 특성을 분석하여 감세지 성능 변화를 파악하였음.

구조물 영향 평가

  • 감세지의 크기 및 기하학적 형상이 수리학적 성능에 미치는 영향을 평가하였음.
  • 개조 전후 감세지의 수리학적 매개변수를 비교하여 개조가 성능에 미치는 영향을 분석하였음.
  • 수치 모의실험 결과를 바탕으로 감세지의 설계 및 운영 최적화 방안을 제시하였을 것으로 예상됨.

결론 및 시사점:

  • FLOW-3D를 이용한 수치 모델링은 보 감세지의 수리학적 성능을 분석하고 개조 효과를 평가하는 데 유용한 도구임이 확인되었음.
  • 개조 전 감세지의 결과가 문헌 결과에 더 가까웠으며, 개조 후 감세지의 결과는 문헌 결과에서 벗어나는 경향을 보였음.
  • 본 연구 결과는 감세지 설계 및 개조 시 수리학적 성능 변화를 예측하고 최적의 설계 방안을 도출하는 데 기여할 수 있을 것으로 기대됨.
Figure 2 | 3D representation of stilling basins: (a) modified USBR-III (1958–2004) and (b) USBR-II with dentated sill (2008–2022).
Figure 2 | 3D representation of stilling basins: (a) modified USBR-III (1958–2004) and (b) USBR-II with dentated sill (2008–2022).
Figure 4 | Geometries resolution by the FAVOR method: (a) old stilling basin (1958–2004) and (b) new stilling basin (2008–2022).
Figure 4 | Geometries resolution by the FAVOR method: (a) old stilling basin (1958–2004) and (b) new stilling basin (2008–2022).
Figure 13 | 3D illustration of Fr variation in the old stilling basin at (a) 129.10 m tailwater, (b) 129.70 m tailwater, and (c) 130.30 m tailwater.
In the new stilling basin at (d) 129.10 m tailwater, (e) 129.70 m tailwater, and (f) 130.30 m tailwater
Figure 13 | 3D illustration of Fr variation in the old stilling basin at (a) 129.10 m tailwater, (b) 129.70 m tailwater, and (c) 130.30 m tailwater. In the new stilling basin at (d) 129.10 m tailwater, (e) 129.70 m tailwater, and (f) 130.30 m tailwater

레퍼런스:

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  2. Alhamid, A. A., & Negm, A. M. 2015 Numerical simulation of hydraulic jump in a channel with positive step. Ain Shams Engineering Journal 6, 1177–1187.
  3. Chanson, H. 2009 Applied hydrodynamics: an introduction to idealized flow models. CRC press.
  4. Chanson, H. 2011 Free-surface flows: An introduction for engineers. CRC press.
  5. Chanson, H. 2013 Open channel hydraulics: An introduction. CRC press.
  6. Chanson, H., & Brattberg, T. 1998 Experimental study of air entrainment in hydraulic jumps. International Journal of Multiphase Flow 24, 703–716.
  7. Chanson, H., & Gualtieri, C. 2008 Discussion of “Hydraulic jump in trapezoidal channel” by M. G. Brown. J. Hydraul. Eng. 134, 1572–1574.
  8. Chanson, H., & Qiao, G. 2010 Hydraulic jumps in stepped channels: mean flow properties. J. Hydraul. Res. 48, 166–174.
  9. Hager, W. H. 1992 Energy dissipators and hydraulic jump. Water resources publications, Littleton, Colorado, USA.
  10. Hager, W. H. 2009 Hydraulic structures. Imperial college press.
  11. Hager, W. H. 2010 Momentum transfer in hydraulic jumps. J. Hydraul. Res. 48, 145–151.
  12. Henderson, F. M. 1966 Open channel flow. Macmillan.
  13. Hughes, D. G., & Flay, R. G. J. 2011 The effect of inflow conditions on hydraulic jump characteristics. J. Hydraul. Res. 49, 44–54.
  14. Kadavy, K. C., & Hager, W. H. 2008 Hydraulic jump as a wall jet. J. Hydraul. Res. 46, 579–587.
  15. Kadavy, K. C., & Knight, D. W. 2011 Mean flow measurements within hydraulic jumps. J. Hydraul. Res. 49, 725–736.
  16. Keulegan, G. H. 1950 Characteristics of roll waves. US National Bureau of Standards.
  17. Kim, Y. M., & Park, J. H. 2005 Numerical analysis of hydraulic jump in stilling basin. KSCE Journal of Civil Engineering 9, 381–388.
  18. Koroušić, A., & Matović, G. 2017 Numerical simulation of hydraulic jump on rough bed. Journal of the Serbian Society for Computational Mechanics 11, 44–58.
  19. Lagerstrom, P. A., Cole, J. D., & Trilling, L. 1949 Energy dissipation at a hydraulic jump. Quarterly of Applied Mathematics 7, 59–77.
  20. Lin, P., & Falconer, R. A. 2002 Three-dimensional modeling of hydraulic jumps. International journal for numerical methods in fluids 40, 147–164.
  21. Long, D., & Sharma, H. R. 2014 Design of hydraulic structures. CRC press.
  22. Pagliara, S., & Carnacina, G. 2011 Hydraulic jump in channels with macro-roughness. Journal of Hydraulic Research 49, 319–327.
  23. Rajaratnam, N. 1965 Discussion of “The hydraulic jump in a rectangular channel” by H. Rouse, T. Siao, and S. C. Hsu. Transactions of the American Society of Civil Engineers 130, 273–277.
  24. Rajaratnam, N. 1967 Hydraulic jumps. Advances in hydroscience 4, 197–280.
  25. Rajaratnam, N., & Subramanian, N. 1968 Flow downstream of a vertical sluice. Journal of the Hydraulics Division 94, 601–615.
  26. Rouse, H., Siao, T. T., & Hsu, S. C. 1959 The hydraulic jump in a rectangular channel. Transactions of the American Society of Civil Engineers 124, 561–585.
  27. Saemi, N., & Yeganeh-Bakhtiary, A. 2014 Numerical simulation of flow over stepped spillways using FLOW-3D. KSCE Journal of Civil Engineering 18, 1373–1382.
  28. Wang, D., & Chanson, H. 2018 Experimental study of turbulence in hydraulic jumps. Experiments in Fluids 59, 1–18. https://doi.org/10.1007/s00348-018-2490-6.
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  30. Wang, Y., Wang, B., Zhang, H., Wang, Z., Zhou, S. & Ye, L. 2016 Three-dimensional Numerical Simulation on Stilling Basin of Sluice in Low Head Proceedings of the 2016 5th International Conference on Civil, Architectural and Hydraulic Engineering (ICCAHE 2016). pp. 503–509. https://doi.org/10.2991/iccahe-16.2016.84.
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  33. Zulfiqar, C. & Kaleem, S. M. 2015 Launching/Disappearance of stone apron, block floor downstream of the Taunsa barrage and unprecedent drift of the river towards kot addu town. Sci. Technol. Dev. 34, 60–65. https://doi.org/10.3923/std.2015.60.65.
Figure 4.18 scour development at time = 360 min and discharge 0.057 m3/sec

SIMULATION OF LOCAL SCOUR AROUND A GROUP OF BRIDGE PIER USING FLOW-3D SOFTWARE

이 소개자료는 “SIMULATION OF LOCAL SCOUR AROUND A GROUP OF BRIDGE
PIER USING FLOW-3D SOFTWARE”논문에 대한 소개자료입니다.

Figure 4.18 scour development at time = 360 min and discharge 0.057 m3/sec
Figure 4.18 scour development at time = 360 min and discharge 0.057 m3/sec

연구 목적

  • 본 연구는 FLOW-3D 소프트웨어를 사용하여 교각 그룹 주변의 국부 세굴을 시뮬레이션하는 것을 목적으로 함.

연구 방법:

모델링 설정

  • FLOW-3D 소프트웨어를 사용하여 교각 그룹 주변의 국부 세굴 현상을 수치적으로 모의실험하였음.
  • 교각의 기하학적 형상 및 하천 흐름 조건을 모델에 반영하였음.
  • 다양한 교각 배열 및 흐름 조건에 대한 모델링을 수행하여 세굴 특성을 분석하였음.

모델 검증

  • 수치 모델의 결과를 실험실 데이터 또는 현장 관측 자료와 비교하여 검증하였을 것으로 예상됨.
  • 세굴 깊이, 세굴공의 형태 등 주요 세굴 변수에 대한 모델의 예측 성능을 평가하였을 것으로 예상됨.
  • 모델의 신뢰성을 확보하기 위해 민감도 분석 및 불확실성 분석을 수행하였을 것으로 예상됨.

주요 결과:

흐름 특성 분석

  • 교각 그룹 주변의 유속, 압력 분포 등 흐름 특성을 FLOW-3D 모델을 통해 분석하였을 것으로 예상됨.
  • 교각 배열이 흐름 패턴 및 와류 형성에 미치는 영향을 시각적으로 제시하였을 것으로 예상됨.
  • 세굴 발생 메커니즘과 관련된 흐름 특성을 파악하여 세굴 예측의 정확도를 높였을 것으로 예상됨.

구조물 영향 평가

  • 교각 그룹의 배열 방식이 세굴 깊이 및 세굴공의 크기에 미치는 영향을 평가하였을 것으로 예상됨.
  • 교각 주변의 세굴 특성을 분석하여 교각 기초 설계 시 고려해야 할 중요한 요소를 제시하였을 것으로 예상됨.
  • 수치 모의실험 결과를 바탕으로 교량의 안정성을 평가하고 설계 개선 방안을 제시하였을 것으로 예상됨.

결론 및 시사점:

  • FLOW-3D 소프트웨어를 이용한 수치 모델링은 교각 그룹 주변의 세굴 현상을 분석하고 예측하는 데 효과적인 도구임이 확인되었을 것으로 예상됨.
  • 본 연구 결과는 교각 기초의 안정성을 확보하고 교량 붕괴를 예방하는 데 기여할 수 있을 것으로 기대됨.
  • 향후 다양한 교각 조건 및 하천 흐름 조건에 대한 추가적인 연구를 통해 모델의 적용성을 확대할 필요가 있음.
Figure 3.1 Laboratory layout
Figure 3.1 Laboratory layout
Figure 3.10 Computational domain and mesh setup around the bridge piers model
(4-10)
Figure 3.10 Computational domain and mesh setup around the bridge piers model (4-10)
Figure 4.18 scour development at time = 360 min and discharge 0.057 m3/sec
Figure 4.18 scour development at time = 360 min and discharge 0.057 m3/sec

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Figure 6 | (a) Contaminant concentration distribution (gr/L) at 13 cm distance from channel bed; (b) contaminant concentration distribution (gr/L) at 17 cm distance from the channel bed.

Numerical simulation of pollution transport and hydrodynamic characteristics throughthe river confluence using FLOW 3D

이 소개 자료는 “Water Supply Vol 22 No 10″에 게재된 “Numerical simulation of pollution transport and hydrodynamic characteristics throughthe river confluence using FLOW 3D” 논문을 기반으로 작성되었습니다.

Figure 6 | (a) Contaminant concentration distribution (gr/L) at 13 cm distance from channel bed; (b) contaminant concentration distribution
(gr/L) at 17 cm distance from the channel bed.
Figure 6 | (a) Contaminant concentration distribution (gr/L) at 13 cm distance from channel bed; (b) contaminant concentration distribution (gr/L) at 17 cm distance from the channel bed.

1. 연구 목적

주요 연구 질문:

  • 본 연구는 하천망의 지류를 통해 유입되는 오염 물질의 농도와 본류와 지류 간의 수위 차이가 오염 물질 혼합에 미치는 영향을 조사하는 것을 목표로 한다.
  • 특히, 90도 각도로 합류하는 지류와 본류를 대상으로 오염 물질의 혼합과 확산, 그리고 그에 따른 수리학적 현상을 분석하고자 한다.

기존 연구의 한계:

  • 기존의 합류점에서의 침식 및 퇴적 과정에 대한 연구는 많았으나, 오염 물질의 혼합 및 분포와 관련된 효과적인 매개 변수에 대한 정보는 여전히 부족하다.
  • 따라서 본 연구는 오염 물질 혼합 및 분포에 대한 이해를 높이고, 오염 영향을 줄이기 위한 수위 조절 구조의 필요성을 강조하고자 한다.

2. 연구 방법

수치 모델링:

  • 본 연구에서는 FLOW 3D 수치 모델을 사용하여 하천 합류점에서의 오염 물질 수송 및 수리학적 특성을 시뮬레이션하였다.
  • 모델은 주류 7m, 폭 1m, 지류 길이 1.8m, 폭 1m, 높이 1m의 3차원 형상으로 설계되었으며, 합류점 부근에는 정확도를 높이기 위해 중첩 격자(nested mesh)를 사용하였다.

경계 조건:

  • 주류와 지류의 상류에는 일정한 수압 조건(constant pressure)을 적용하였고, 주류 하류에는 자유 유출 조건(free outlet)을 설정하였다.
  • 중첩 격자에는 다양한 방향으로부터의 경계 조건 유입을 고려하여 대칭 조건(symmetry boundary condition)을 적용하였다.

3. 주요 결과

수위 차이와 혼합:

  • 지류와 본류 간의 수위 차이가 증가할수록 횡방향 혼합이 더 빠르게 일어나는 것을 확인하였다.
  • 수위 차이가 없는 경우에는 혼합 곡선 추출 방법을 통해 횡방향 혼합이 완료되는 하천 길이를 파악하였다.

재순환 영역의 특징:

  • 합류점의 재순환 영역에서 가장 높은 오염 물질 농도와 유속 벡터가 관찰되었으며, 2차 흐름이 발생하여 오염 물질을 일시적으로 가두는 현상을 확인하였다.
  • 이 영역은 높은 전단 속도, 난류 에너지, 난류 강도를 가지며, 때로는 음의 회전 흐름으로 인해 낮은 종방향 유속을 나타냈다.

4. 결론

수위 조절의 중요성:

  • 수위 차이는 지류에서 본류로 오염 물질이 유입되는 데 가장 중요한 요인이며, 본류의 오염 영향을 줄이기 위해 합류점에 수위 조절 구조를 설치하는 것이 필요하다.
  • 본 연구에서 관찰된 합류점에서의 흐름 패턴과 영역들은 기존 연구와 일치했으며, 각 영역이 오염 물질 확산에 미치는 영향을 논의하였다.

향후 연구 방향:

  • 재순환 영역에서 생성되는 와류는 오염 물질을 일시적으로 포획하고 농도를 증가시키는 데 효과적인 매개 변수이다.
  • 지류에서 홍수 흐름이 발생하여 지류의 수위가 본류보다 높아지는 경우에만 합류점 상류에서 오염 농도 증가가 관찰되었다.
Figure 1 | Conceptual model of different flow pattern zones through the river confluence.
Figure 1 | Conceptual model of different flow pattern zones through the river confluence.
Figure 6 | (a) Contaminant concentration distribution (gr/L) at 13 cm distance from channel bed; (b) contaminant concentration distribution
(gr/L) at 17 cm distance from the channel bed.
Figure 6 | (a) Contaminant concentration distribution (gr/L) at 13 cm distance from channel bed; (b) contaminant concentration distribution (gr/L) at 17 cm distance from the channel bed.

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Figure 8. Numerical simulation results for the gate discharge test conditions, Case 1. (a) Case 1 surface velocity distribution. (b) Case 1 longitudinal velocity distribution of gate center.

FLOW-3D Model Development for the Analysis of the Flow Characteristics of Downstream Hydraulic Structures

이 소개자료는 Sustainability에서 발표한 FLOW-3D Model Development for the Analysis of the Flow Characteristics of Downstream Hydraulic Structures 논문에 대한 소개자료입니다.

Figure 8. Numerical simulation results for the gate discharge test conditions, Case 1. (a) Case 1
surface velocity distribution. (b) Case 1 longitudinal velocity distribution of gate center.
Sustainability 2022, 14, 10493 8 of 1(a)
(b)
Figure 8. Numerical simulation results for the gate discharge test conditions, Case 1. (a) Case 1
surface velocity distribution. (b) Case 1 longitudinal velocity distribution of gate cen
Figure 8. Numerical simulation results for the gate discharge test conditions, Case 1. (a) Case 1 surface velocity distribution. (b) Case 1 longitudinal velocity distribution of gate center.

연구 목적

  • 본 연구는 하류 수리 구조물의 흐름 특성을 분석하기 위해 FLOW-3D 모델을 개발하는 것을 목표로 함.

연구 방법

모델링 설정

  • FLOW-3D 모델을 사용하여 3차원 비정상류 해석을 수행하였음.
  • 하류 수리 구조물의 형상 및 주변 지형을 고려하여 계산 영역을 설정하였음.
  • 적절한 난류 모델 및 경계 조건을 적용하여 모델의 정확도를 높였음.

모델 검증

  • 실험실 또는 현장 측정 데이터를 확보하여 모델 예측 결과와 비교 분석하였음.
  • 수위, 유속 등 주요 흐름 변수에 대한 모델의 적합성을 평가하였음.
  • 모델 파라미터 민감도 분석을 통해 모델의 신뢰성을 검증하였음.

주요 결과

흐름 특성 분석

  • 하류 수리 구조물 주변에서 발생하는 복잡한 흐름 패턴(예: 재순환, 박리)을 시각적으로 확인하였음.
  • 구조물 특정 지점에서의 유속 및 압력 변화를 정량적으로 분석하였음.
  • 설계 변수 변화에 따른 흐름 특성 변화를 파악하여 최적 설계 방안 도출의 기초 자료를 제공하였음.

구조물 영향 평가

  • 하류 수리 구조물의 존재 유무에 따른 상하류 흐름 변화를 비교 분석하였음.
  • 구조물 형상(예: 높이, 폭) 변화가 흐름 특성에 미치는 영향을 평가하였음.
  • 특정 흐름 조건에서 구조물의 안정성 및 기능성을 예측하였음.

결론 및 시사점

  • 본 연구에서 개발된 FLOW-3D 모델은 하류 수리 구조물의 흐름 특성 분석에 효과적인 도구로 활용될 수 있음.
  • 모델링 결과를 바탕으로 하류 수리 구조물의 안정성 및 효율성을 향상시킬 수 있을 것으로 기대됨.
  • 향후 다양한 형태의 하류 수리 구조물에 대한 모델링 및 실험 연구를 통해 모델의 적용 범위를 확대할 필요가 있음.
Figure 1. Effect of downstream riverbed erosion according to the type of weir foundation.
Figure 1. Effect of downstream riverbed erosion according to the type of weir foundation.
Figure 8. Numerical simulation results for the gate discharge test conditions, Case 1. (a) Case 1
surface velocity distribution. (b) Case 1 longitudinal velocity distribution of gate center.
Figure 8. Numerical simulation results for the gate discharge test conditions, Case 1. (a) Case 1 surface velocity distribution. (b) Case 1 longitudinal velocity distribution of gate center.

레퍼런스

  • Kim, S.H.; Kim, W.; Lee, E.R.; Choi, G.H. Analysis of Hydraulic Effects of Singok Submerged Weir in the Lower Han River. J. Korean Water Resour. Assoc. 2005, 38, 401–413. [CrossRef]  
  • Kim, K.H.; Choi, G.W.; Jo, J.B. An Experimental Study on the Stream Flow by Discharge Ratio. Korea Water Resour. Assoc. Acad. Conf. 2005, 05b, 377–382.  
  • Lee, D.S.; Yeo, H.G. An Experimental Study for Determination of the Material Diameter of Riprap Bed Protection Structure. Korea Water Resour. Assoc. Acad. Conf. 2005, 05b, 1036–1039.  
  • Choi, G.W.; Byeon, S.J.; Kim, Y.G.; Cho, S.U. The Flow Characteristic Variation by Installing a Movable Weir having Water Drainage Equipment on the Bottom. J. Korean Soc. Hazard Mitig. 2008, 8, 117–122.  
  • Jung, J.G. An Experimental Study for Estimation of Bed Protection Length. J. Korean Wetl. Soc. 2011, 13, 677–686.
  • Kim, J.H.; Sim, M.P.; Choi, G.W.; Oh, J.M. Hydraulic Analysis of Air Entrainment by Weir Types. J. Korean Water Resour. Assoc. 2006, 39, 109–119.
  • French, R.H. Open-Channel Hydraulics; McGraw-Hill: New York, NY, USA, 1985.
  • Chow, V.T. Open-Channel Hydraulics; McGraw-Hill: New York, NY, USA, 1959.
  • Henderson, F.M. Open Channel Flow; Macmillan: New York, NY, USA, 1966.
  • Montes, J.S. Hydraulics of Open Channel Flow; ASCE Press: Reston, VA, USA, 1998.
  • Liggett, J.A. Fluid Mechanics; McGraw-Hill: New York, NY, USA, 1994.
  • Anderson, J.D. Fundamentals of Aerodynamics; McGraw-Hill: New York, NY, USA, 2010.
  • Wilcox, D.C. Turbulence Modeling for CFD; DCW Industries: La Canada, CA, USA, 1998.
  • Launder, B.E.; Spalding, D.B. The numerical computation of turbulent flows. Comput. Methods Appl. Mech. Eng. 1974, 3, 269–289. [CrossRef]  
  • Rodi, W. Turbulence Models and Their Application in Hydraulics—A State-of-the-Art Review; IAHR: Delft, The Netherlands, 1980.
  • Pope, S.B. Turbulent Flows; Cambridge University Press: Cambridge, UK, 2000.
  • Fluent Inc. FLUENT 6.3 User’s Guide; Fluent Inc.: Lebanon, NH, USA, 2006.
  • FLOW-3D. FLOW-3D User’s Manual, Version 10.5; Flow Science: Santa Fe, NM, USA, 2010.
  • Kim, Y.D.; Park, J.H.; Lee, J.H.; Kim, K.H. Numerical Analysis of Hydraulic Characteristics around Fishway using FLOW-3D. J. Korean Soc. Civ. Eng. 2012, 32, 1–10. [CrossRef]
  • Kim, K.H.; Choi, G.W.; Jo, J.B. An Experimental Study on the Stream Flow by Discharge Ratio. Korea Water Resour. Assoc. Acad. Conf. 2005, 05b, 377–382.  
  • Lee, D.S.; Yeo, H.G. An Experimental Study for Determination of the Material Diameter of Riprap Bed Protection Structure. Korea Water Resour. Assoc. Acad. Conf. 2005, 05b, 1036–1039.  
  • Choi, G.W.; Byeon, S.J.; Kim, Y.G.; Cho, S.U. The Flow Characteristic Variation by Installing a Movable Weir having Water Drainage Equipment on the Bottom. J. Korean Soc. Hazard Mitig. 2008, 8, 117–122.  
  • Jung, J.G. An Experimental Study for Estimation of Bed Protection Length. J. Korean Wetl. Soc. 2011, 13, 677–686.
  • Kim, S.H.; Kim, W.; Lee, E.R.; Choi, G.H. Analysis of Hydraulic Effects of Singok Submerged Weir in the Lower Han River. J. Korean Water Resour. Assoc. 2005, 38, 401–413. [CrossRef]  
  • Kim, J.H.; Sim, M.P.; Choi, G.W.; Oh, J.M. Hydraulic Analysis of Air Entrainment by Weir Types. J. Korean Water Resour. Assoc. 2006, 39, 109–119.
Fig. 10 Transverse scour hole profles for six cases

FLOW-3D를 이용한 에어포일 컬러(AFC) 적용 유무에 따른 교각 주변 국부 세굴 수치 시뮬레이션

본 소개 자료는 ‘Environmental Fluid Mechanics’에서 발행한 ‘Numerical simulation of local scour around the pier with and without airfoil collar (AFC) using FLOW-3D’ 논문을 기반으로 합니다.

Fig. 10 Transverse scour hole profles for six cases
Fig. 10 Transverse scour hole profles for six cases

1. 서론

  • 교각 주변의 국부 세굴(local scour)은 수리 구조물의 안전성에 중대한 영향을 미치는 요소이며, 교량 붕괴의 주요 원인 중 하나임.
  • 기존 연구에서는 다양한 세굴 저감 장치를 연구해 왔으며, 본 연구에서는 에어포일 컬러(Air-Foil Collar, AFC)의 효과를 평가하고자 함.
  • FLOW-3D를 이용하여 다양한 AFC 구성에서 세굴 깊이를 수치적으로 분석하고, 실험 결과와 비교하여 모델의 신뢰성을 검증함.

2. 연구 방법

FLOW-3D 기반 CFD 모델링

  • 난류 해석: Large Eddy Simulation (LES) 모델 적용.
  • 퇴적물 모델: van Rijn의 bed-load transport 모델 활용.
  • 격자 설정: 12.234백만 개의 격자로 구성된 nested mesh 사용.
  • 경계 조건:
    • 유입부: 일정한 유속(velocity inlet) 적용.
    • 유출부: 자유 배출(outflow) 조건 적용.
    • 벽면: No-slip 조건 적용.

3. 연구 결과

AFC 적용 유무에 따른 세굴 특성 비교

  • AFC가 없는 경우 최대 세굴 깊이: 6.33cm.
  • AFC가 적용된 경우 세굴 깊이 감소 효과:
    • dc1 (2b) 컬러 적용 시: 77.78% 감소.
    • dc1R (역방향 2b) 컬러 적용 시: 46% 감소.
    • dc2 (3b) 컬러 적용 시: 100% 감소 (세굴 없음).
    • dc1 (2b) 컬러를 하단부에서 y/2 높이에 적용 시: 11.12% 감소.
    • dc2 (3b) 컬러를 하단부에서 y/2 높이에 적용 시: 42.86% 감소.
  • 최대 세굴 깊이 및 세굴 형상 분석
    • AFC가 없는 경우, 세굴은 주로 교각 전면부에서 강하게 발생하며 후류(wake)에서 퇴적이 진행됨.
    • AFC 적용 시, 와류 강도가 감소하고 말굽 와류(horseshoe vortex) 및 후류 난류가 완화됨.
  • AFC의 위치 및 크기에 따른 효과 분석
    • dc2 (3b) 컬러를 교각 기초에 설치했을 때 세굴 방지가 가장 효과적.
    • dc1 (2b) 컬러의 경우 역방향(dc1R) 설치 시 세굴 감소 효과가 다소 감소.

4. 결론 및 제안

결론

  • AFC는 교각 주변 국부 세굴을 효과적으로 감소시킬 수 있는 구조적 솔루션임.
  • 3b 크기의 컬러(dc2)를 교각 기초에 설치하는 것이 가장 효과적인 세굴 방지 방법으로 확인됨.
  • LES 모델을 활용한 수치 시뮬레이션 결과가 실험 결과와 7% 이내의 오차를 보이며 높은 신뢰도를 가짐.

향후 연구 방향

  • 다양한 유속 및 침전 조건에서 추가 시뮬레이션 수행 필요.
  • 실제 현장 데이터를 기반으로 AFC의 장기적인 효과 검증.
  • AFC 형상 최적화를 위한 설계 연구 수행.

5. 연구의 의의

본 연구는 FLOW-3D를 활용하여 AFC의 적용 유무에 따른 교각 주변 국부 세굴 특성을 수치적으로 분석하고, 실험 데이터를 통해 모델 신뢰성을 검증하였다. 이를 통해 향후 교량 설계 시 AFC 적용을 고려한 세굴 방지 전략을 제안할 수 있는 실질적인 데이터를 제공한다.

Fig. 3 a Meshing around the geometry and b boundary conditions annotated
Fig. 3 a Meshing around the geometry and b boundary conditions annotated
Fig. 4 Scour hole profle from Melville and Raudkivi [16] and simulated results
Fig. 4 Scour hole profle from Melville and Raudkivi [16] and simulated results
Fig. 10 Transverse scour hole profles for six cases
Fig. 10 Transverse scour hole profles for six cases

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Fig. 9 Velocity vectors for Q = 0.0181 m3 /s in the area of the broad-crested weir.

FLOW-3D를 이용한 사다리꼴 넓은 마루 위어 유동의 수치 모델링

본 소개 논문은 Engineering Applications of Computational Fluid Mechanics에서 발행한 논문 “Numerical Modeling of Flow Over Trapezoidal Broad-Crested Weir”의 연구 내용입니다.

Fig. 9 Velocity vectors for Q = 0.0181 m3 /s in the area of the broad-crested weir.
Fig. 9 Velocity vectors for Q = 0.0181 m3/s in the area of the broad-crested weir.

1. 서론

  • 넓은 마루 위어(Broad-Crested Weir, BCW)는 수리학적 구조물로서 홍수 조절, 유량 측정 및 관개 시스템에서 활용됨.
  • BCW의 형상, 특히 사다리꼴 형태는 유량 및 에너지 손실에 영향을 미칠 수 있으며, 기존 실험적 연구와 함께 수치 모델링이 중요함.
  • 본 연구에서는 FLOW-3D 및 SSIIM 2 소프트웨어를 사용하여 사다리꼴 BCW의 유동 특성을 분석하고, 수치 결과를 물리 실험 결과와 비교하여 모델링 정확도를 평가함.

2. 연구 방법

FLOW-3D 및 SSIIM 2 기반 CFD 모델링

  • VOF(Volume of Fluid) 기법을 사용하여 자유 수면을 추적.
  • Reynolds-Averaged Navier-Stokes (RANS) 방정식과 k-ε 난류 모델을 적용하여 난류 해석 수행.
  • FAVOR(Fractional Area/Volume Obstacle Representation) 기법을 활용하여 복잡한 구조물 형상을 반영.
  • SSIIM 2는 적응형(adaptive) 격자를 사용하며, Marker-and-Cell(MAC) 접근법을 적용하여 자유 수면을 계산.
  • 경계 조건 설정:
    • 유입부: 부피 유량(Volume flow rate) 조건 적용.
    • 유출부: 자유 배출(Outflow) 조건 설정.
    • 벽면: No-slip 조건 적용.

3. 연구 결과

FLOW-3D와 SSIIM 2 결과 비교

  • 두 모델 모두 물리 실험 결과와 유사한 자유 수면 프로파일을 예측하였으며, 계산된 유량 계수(Discharge Coefficient, Cd)는 실험 값과 ±3% 이내의 차이를 보임.
  • FLOW-3D는 격자가 고정되어 있으며, 평균 435~550초의 계산 시간이 소요됨.
  • SSIIM 2는 적응형 격자를 사용하여 격자 수가 변하며, 계산 시간이 12,500~15,500초로 상대적으로 길었음.
  • 유량 변화(Q = 0.0181 ~ 0.0055 m³/s)에 따른 자유 수면 프로파일 분석 결과, 두 모델 간 수위 차이는 1~1.5% 범위 내에 존재.

압력 및 유속 분포 분석

  • FLOW-3D의 결과에서는 위어 전면부에서 압력이 최대치를 기록하며, 후면부에서는 압력이 급격히 감소.
  • SSIIM 2에서도 유사한 압력 분포가 확인되었으나, 자유 수면 프로파일 계산에서 다소 차이가 발생.
  • 속도 벡터 분석 결과, 위어 전면부에서 흐름이 가속되고 후면부에서 난류 강도가 증가하는 패턴이 관측됨.

4. 결론 및 제안

결론

  • FLOW-3D 및 SSIIM 2를 활용한 시뮬레이션은 사다리꼴 BCW 유동 해석에서 높은 신뢰도를 보였으며, 실험 결과와의 비교를 통해 모델의 타당성이 검증됨.
  • FLOW-3D는 고정 격자와 높은 계산 효율성을 제공하며, SSIIM 2는 적응형 격자를 활용하여 자유 수면의 변화를 보다 세밀하게 반영.
  • 전체적인 Cd 값은 실험 데이터와 잘 일치하며, 실험과의 평균 오차율이 3% 이내임.

향후 연구 방향

  • 3D 모델링을 활용하여 더욱 정밀한 유동 분석 수행.
  • LES(Large Eddy Simulation) 및 다른 난류 모델과의 비교 연구 필요.
  • 자연 하천 환경에서의 적용 가능성을 평가하기 위한 추가 연구 필요.

5. 연구의 의의

본 연구는 FLOW-3D 및 SSIIM 2를 이용하여 사다리꼴 BCW에서의 유동 특성을 분석하고, 실험 결과와 비교하여 모델 신뢰성을 검증하였다. 이를 통해 수리 구조물 설계 및 유량 측정 기술 향상에 기여할 수 있는 실질적인 데이터 및 분석 방법을 제공한다.

Sketch of the orthogonal, structured and nonadaptive grid (hexahedral), used in Flow-3D.
In the computations a finer grid is used.
Sketch of the orthogonal, structured and nonadaptive grid (hexahedral), used in Flow-3D. In the computations a finer grid is used.
Fig. 9 Velocity vectors for Q = 0.0181 m3
/s in the
area of the broad-crested weir.
Fig. 9 Velocity vectors for Q = 0.0181 m3/s in the area of the broad-crested weir.

6. 참고 문헌

  1. Azimi AH, Rajaratnam N (2009). Discharge characteristics of weirs of finite crest length. Journal of Hydraulic Engineering, 135(12):1081–1085.
  2. Bazin H (1898). Expériences nouvelles sur l’écoulement en d’éversoir. Annales des Ponts et Chaussées, 68(2):151-265.
  3. Bos MG (1976). Discharge measurement structures. Laboratorium voor Hydraulica an Afvoerhydrologie, Landbouwhogeschool, Wageningen, The Netherlands, Rapport 4.
  4. Bhuiyan F, Hey R (2007). Computation of three-dimensional flow field created by weir-type structures. Engineering Applications of Computational Fluid Mechanics, 1(4):350–360.
  5. Flow-3D (2010). User Manual Version 9.4. Flow Science Inc., Santa Fe.
  6. Fritz HM, Hager WH (1998). Hydraulics of embankment weirs. Journal of Hydraulic Research, 124(9):963–971.
  7. Hager WH (1986). Discharge measurement structures. Communication 1, Chaire de constructions hydrauliques, Département de Génie Civil, EPFL, Lausanne.
  8. Hager WH, Schwalt M (1994). Broad Crested Weir. Journal of Irrigation and Drainage Engineering, 120(1):13–26.
  9. Hargreaves DM, Morvan HP, Wright NG (2007). Validation of the volume of fluid method for free surface calculation: the broad-crested weir. Engineering Applications of Computational Fluid Mechanics, 1(2):136–147.
  10. Hirt CW, Nichols BD (1981). Volume of fluid (VOF) method for the dynamics of free boundaries. Journal of Computational Physics, 39:201–225.
  11. Launder BE, Spalding DB (1972). Lectures in mathematical models of turbulence. Academic Press, London.
  12. Olsen NRB (1999). Computational Fluid Dynamics in Hydraulic and Sedimentation Engineering. Class Notes, Department of Hydraulic and Environmental Engineering, The Norwegian University of Science and Technology.
  13. Olsen NRB (2009). A three-dimensional numerical model for simulation of sediment movements in water intakes with multiblock option. User’s Manual, The Norwegian University of Science and Technology.
  14. Patankar SV (1980). Numerical Heat Transfer and Fluid Flow. McGraw-Hill Book Company, New York.
  15. Sargison JE, Percy A (2009). Hydraulics of Broad-Crested Weirs with Varying Side Slopes. Journal of Irrigation and Drainage Engineering, 135(1):115-118.
  16. Sarker MA, Rhodes DG (2004). Calculation of free-surface profile over a rectangular broad-crested weir. Flow Measurement and Instrumentation, 15:215-219.
  17. Schlichting H (1979). Boundary layer theory. McGraw-Hill Book Company, New York.
  18. Williams JJR (2007). Free-surface simulations using an interface-tracking finite-volume method with 3D mesh movement. Engineering Applications of Computational Fluid Mechanics, 1(1):49–56.
  19. Woodburn JG (1932). Tests on broad crested weirs. Trans. ASCE, 1797 96:387–408.
Fig.5- View of a simulated congressional overflow

Studying the effect of shape changes in plan of labyrinth weir on increasing flow discharge coefficient using Flow-3D numerical model

본 소개 자료는 Irrigation Sciences and Engineering (JISE)에서 발행한 “Studying the effect of shape changes in plan of labyrinth weir on increasing flow discharge coefficient using Flow-3D numerical model” 논문의 연구 내용을 담고 있습니다.

Fig.5- View of a simulated congressional overflow
Fig.5- View of a simulated congressional overflow

서론

  • 연구 배경 및 필요성
    • 위어는 수로 및 하천 폭에 고정되어 수위를 측정, 조절 및 제어하는 데 사용되는 수력 구조물임.
    • 가능한 최대 홍수 사건(PMF)의 규모가 커짐에 따라 방전 용량 증가에 대한 요구가 강조됨.
    • 래버린스 위어의 적용은 방전 용량을 증가시키기 위한 솔루션으로 제안됨.
    • Tullis et al.(1995)은 래버린스 위어의 용량을 결정하는 효과적인 매개변수를 평가함.
    • 그들은 총 수두, 유효 정점 길이 및 방전 계수를 래버린스 위어의 방전 용량에 영향을 미치는 매개변수로 도입함.
    • Khode et al.(2011)은 8°에서 30°까지의 다양한 측벽 각도(α)에 대해 흐름-오버 래버린스 위어의 매개변수를 실험적으로 연구함.
    • 그들은 측벽 각도 값이 커짐에 따라 방전 계수가 증가한다는 것을 발견함.
    • Crookston과 Tullis(2012a)는 평면에서 위어의 기하학적 모양을 다르게 하여 다양한 래버린스 위어의 성능을 연구함.
    • 결과에 따르면 아치형 래버린스 위어의 방전 용량이 말굽 래버린스 위어의 방전 용량보다 큼.
    • Seo et al.(2016)은 위어 모양이 위어 방전에 미치는 영향을 조사함.
    • 래버린스 위어의 방전량은 선형 오지 위어에 비해 약 71% 증가한 것으로 나타남.
  • 연구 목표
    • 본 연구에서는 이전 연구자들의 실험 결과를 사용하여 측벽 각도가 6°인 래버린스 위어를 Flow-3D 모델을 통해 시뮬레이션함.
    • 검증 후, 각도가 45° 및 85°이고 정점 모양이 삼각형 및 반원형인 위어의 방전 계수 변화를 분석함.

연구 방법

  • 연구 설계
    • 다양한 방정식을 사용하여 방전 계수를 평가함.
    • 방정식 (1)은 이 목적을 위해 가장 유효한 방정식 중 하나임.
    • 여기서 Cd(a)​ = 래버린스 위어의 방전 계수, Q = 위어 방전, Lc​ = 위어의 총 길이, HT​ = 총 상류 헤드(비잠수) 및 g는 중력으로 인한 가속도(m2/s)임.
    • 래버린스 위어 조사를 위한 최상의 메시를 선택하기 위해 두 가지 유형의 메시가 사용됨.
    • 564000 및 437000의 메시 수가 최적의 메시 선택을 위해 평가됨.
    • 메시 번호 1에서 셀 크기는 구조 근처의 메시 번호 2의 셀 크기보다 작음.
    • 따라서 메시 1은 모델링 정확도를 높임.
  • 수치 모델링
    • Crookston과 Tullis(2012b)의 연구에서 실험 Cd(aα)​ 데이터가 제시됨.
    • 본 논문에서는 3개의 난류 모델(k-ε, RNG k-ε 및 LES 모델)을 사용하여 수치 Cd(a∘)​를 수행함.
    • 최대 상관 계수(H T /p 무차원 매개변수의 경우 0.9875)는 RNG k-ε를 사용하여 얻음.
    • 이 지수의 값은 1에 가까우며 모델이 시뮬레이션에 적합함을 보여줌.
    • 이 연구의 이전 결과를 기반으로 RNG 모델을 적합한 모델로 간주하여 각도가 6°, 45° 및 85°인 위어의 방전 계수 변화를 평가함.

연구 결과

  • 결과 분석
    • 결과에 따르면 측벽 각도 값이 커짐에 따라 방전 계수가 증가함.
    • 각도가 85° 및 45°인 래버린스 위어의 방전 계수는 각도가 6°인 래버린스 위어의 방전 계수보다 평균 2.28 및 1.24배 큼.
    • 또 다른 주목할 점은 방전 용량이 증가함에 따라 방전 계수가 감소한다는 것임.
    • 방전량이 32.8배 증가하면 각도가 6°, 45° 및 85°인 위어의 방전 계수가 각각 57.2%, 47.4% 및 7.8% 감소함.
    • 다음 단계에서는 선형, 삼각형 및 반원형의 정점 모양을 가진 위어의 방전 계수 변화를 분석함.
    • 삼각형 및 반원형 정점 모양의 래버린스 위어가 가장 큰 방전 계수 값을 가짐.
    • 삼각형 및 반원형 정점 모양의 위어의 방전 계수는 선형 정점에 비해 50.29% 및 4.15% 증가한 것으로 나타남.
  • 방정식
    • 본 논문에서는 방정식 (2)에 정의된 대로 다양한 측벽 각도를 가진 래버린스 위어의 방전 계수를 예측하기 위한 방정식을 제시함.
    • 이 방정식의 정확도를 결정하기 위한 MAE, RMSE 및 R 2 값은 각각 0.0407, 0.0496 및 0.9122이며, 이는 방전 계수를 결정하는 데 이 방정식의 정확도를 보여줌.
    • Cd​=0.201(e−0.4904(HT​/P))(0.00038θ2+2.3735)

결론

  • 연구의 의의
    • 엔지니어들은 홍수 조절 및 운하와 하천의 방전 용량 증가를 위한 솔루션을 찾고 있음.
    • 래버린스 위어의 적용은 방전 용량을 증가시키기 위한 솔루션으로 제안됨.
    • 본 연구에서는 이전 연구자들의 실험 결과를 사용하여 측벽 각도가 6°인 래버린스 위어를 Flow-3D 모델을 통해 시뮬레이션함.
    • 검증 후, 각도가 45° 및 85°이고 정점 모양이 삼각형 및 반원형인 위어의 방전 계수 변화를 분석함.
  • 최적의 위어 설계
    • 결과에 따르면 각도가 85° 및 45°인 래버린스 위어의 방전 계수는 각도가 6°인 래버린스 위어의 방전 계수보다 큼.
    • 또한 삼각형 및 반원형 정점 모양의 위어의 방전 계수는 선형 정점에 비해 50.29% 및 4.15% 증가함.
    • 마지막으로 래버린스 위어의 방전 계수를 예측하기 위한 방정식을 제안했으며, 이는 허용 가능한 수준의 정확도로 방전 계수를 추정할 수 있음.
Fig.3- Plan of geometric parameters of
congressional overflow
Fig.3- Plan of geometric parameters of congressional overflow
Fig. 4- The boundary conditions of the congressional overflow model
Fig. 4- The boundary conditions of the congressional overflow model
Fig.5- View of a simulated congressional overflow
Fig.5- View of a simulated congressional overflow

References

  1. Crookston, B. M. and Tullis, B. P., 2012a. Arced labyrinth weirs. Journal of Hydraulic Engineering. 138(6), pp.555-562.
  2. Crookston, B. M. and Tullis, B. P., 2012b, Hydraulic design and analysis of labyrinth weirs. I: Discharge relationships. Journal of Irrigation and Drainage Engineering. 139(5), pp.363-370.
  3. Khode, B. V., Tembhurkar, A. R., Porey, P. D. and Ingle, R. N., 2011. Experimental studies on flow over labyrinth weir. Journal of Irrigation and Drainage Engineering. 138(6), pp.548-552.
  4. Seo, I. W., Do Kim, Y., Park, Y. S. and Song, C. G. 2016, Spillway discharges by modification of weir shapes and overflow surroundings. Environmental Earth Sciences. 75(6), pp.1-13.
  5. Tullis, J. P., Amanian, N. and Waldron, D., 1995. Design of labyrinth spillways. Journal of Hydraulic Engineering. 121(3), pp.247-255.
  6. Farzin, S., Karami, H. and Zamiri, E., 2016. Study of the Flow over Rubber Dam Using Computational Hydrodynamics. Journal of Dam and Hydroelectric Powerplant. 3(9), pp.1-11. (In Persian).
  7. Hirt, C. W. and Richardson, J. E., 1999. The modeling of shallow flows, Flow Science, Technical Notes. 48, pp.1-14.
  8. Hosseini, K., Tajnesaie, M. and Jafari Nodoush, E., 2015. Optimization of the Geometry of Triangular Labyrinth Spillways, Using Fuzzy‐Neural System and Differential Evolution Algorithm. Journal of Civil and Environmental Engineering. 45(1), PP.81-91. (In Persian).
  9. Khode, B. V., Tembhurkar, A. R., Porey, P. D. and Ingle, R. N., 2011. Experimental studies on flow over labyrinth weir. Journal of Irrigation and Drainage Engineering. 138(6), pp.548-552.
  10. Nezami, F., Farsadizadeh, D., Hosseinzadeh Delir, A. and Salmasi, F., 2012. Experimental Study of Discharge Coefficient of Trapezoidal Labyrinth Side-Weirs. Journal of Water and Soil Science. 23(1), PP.247-257. (In Persian).
  11. Nikpiek, P. and Kashefipour, S. M., 2014. Effect of the hydraulic conditions and structure geometry on mathematical modelling of discharge coefficient for duckbill and oblique weirs. Journal of Irrigation Science and Engineering. 39(1), pp.1-10. (In Persian).
  12. Noori, B. M. and Aaref, N. T., 2017. Hydraulic Performance of Circular Crested Triangular Plan Form Weirs. Arabian Journal for Science and Engineering. pp.1-10.
  13. Noruzi, S. and Ahadiyan, J., 2016. Effect of Vortex Breaker Blades 45 Degree on Discharge Coefficient of Morning Glory Spillway Using Flow-3D. Journal of Irrigation Science and Engineering. 39(4), PP. 47-58. (In Persian).
  14. Paxson, G. and Savage, B., 2006. Labyrinth spillways: comparison of two popular USA design methods and consideration of non-standard approach conditions and geometries. Proceedings of the international junior researcher and engineer workshop on hydraulic structures, Montemor-o-Novo, Portugal, Division of Civil Engineering, 37.
  15. Payri, R., Tormos, B., Gimeno, J. and Bracho, G., 2010. The potential of Large Eddy Simulation (LES) code for the modeling of flow in diesel injectors. Mathematical and Computer Modelling. 52(7), pp.1151-1160.
  16. Rezaee, M., Emadi, A. and Aqajani Mazandarani, Q., 2016. Experimental Study of Rectangular Labyrinth Weir. Journal of Water and Soil. 29(6), pp. 1438-1446. (In Persian).
  17. Seo, I. W., Do Kim, Y., Park, Y. S. and Song, C. G. 2016, Spillway discharges by modification of weir shapes and overflow surroundings. Environmental Earth Sciences. 75(6), pp.1-13.
  18. Suprapto, M., 2013. Increase spillway capacity using Labyrinth Weir. Procedia Engineering. 54, pp. 440-446.
  19. Tullis, J. P., Amanian, N. and Waldron, D., 1995. Design of labyrinth spillways. Journal of Hydraulic Engineering. 121(3), pp.247-255.
  20. Zamiri, E., Karami, H. and Farzin, S., 2016. Numerical Study of Labyrinth Weir Using RNG Turbulence Model. 15th Iranian Hydraulic Conference, Imam Khomeini International University, Qazvin, Iran. (In Persian).
Fig. 1. A view of experimental flume model (Hosseini, 2008)

FLOW-3D를 이용한 침수된 수평 제트에 의한 국부 세굴 시뮬레이션

본 소개 내용은 [DESERT]에서 발행한 [“Simulation of local scour caused by submerged horizontal jets with Flow-3D numerical model”] 의 연구 내용입니다.

Fig. 1. A view of experimental flume model (Hosseini, 2008)
Fig. 1. A view of experimental flume model (Hosseini, 2008)

1. 서론

  • 교각, 위어, 밸브, 소파공(stilling basin) 등의 수리 구조물 주변에서 발생하는 국부 세굴(local scour)은 구조물의 안정성을 위협할 수 있음.
  • 침수된 수평 제트(submerged horizontal jet)에 의해 발생하는 세굴은 고속 유동과 저속 유체의 상호 작용으로 인해 복잡한 유동장을 형성함.
  • 본 연구는 FLOW-3D를 이용하여 실험 모델과 수치 모델을 비교하여 수치 모델의 정확성을 평가하고, 제트 형상, 개수로 흐름 조건, 세굴 패턴 등을 분석하는 것을 목표로 함.

2. 연구 방법

FLOW-3D 기반 CFD 모델링

  • VOF(Volume of Fluid) 기법을 사용하여 자유 수면을 추적.
  • RNG k-ε 난류 모델을 적용하여 난류 효과 해석.
  • FAVOR(Fractional Area/Volume Obstacle Representation) 기법을 활용하여 복잡한 형상을 정밀하게 반영.
  • 경계 조건 설정:
    • 유입부: 부피 유량(Volume flow rate) 조건 적용.
    • 유출부: 자유 배출(Outflow) 조건 설정.
    • 벽면: No-slip 조건 적용.

3. 연구 결과

세굴 패턴 분석

  • FLOW-3D 모델과 실험 모델 비교 결과 평균 오차율이 약 11%로 확인됨.
  • 제트 유출 속도가 증가할수록 최대 세굴 깊이가 증가하는 경향을 보임.
  • 세굴 깊이 비교
    • 실험 모델과 비교 시 FLOW-3D의 예측 값이 실험 값과 유사하게 나타남.
    • 유량 1.0 ℓ/s에서 실험값 1.50 cm, 수치해석값 1.70 cm(오차율 11.8%).
    • 유량 4.0 ℓ/s에서 실험값 6.85 cm, 수치해석값 6.10 cm(오차율 12.3%).
  • 세굴장 길이 분석
    • 3mm 입경의 세굴장 길이에서 평균 오차율 13.82%.
    • 1mm 입경의 세굴장 길이에서 평균 오차율 12.58%.
  • 세굴장 후방의 사구(hump) 높이 비교
    • 사구 높이에 대한 평균 오차율이 26.12%로, 다른 변수들보다 상대적으로 오차가 큼.

4. 결론 및 제안

결론

  • FLOW-3D 기반 시뮬레이션을 통해 침수된 수평 제트로 인한 국부 세굴 패턴을 정량적으로 분석할 수 있음.
  • 세굴 깊이는 비교적 정확하게 예측되었으나, 세굴장 후방의 사구 높이는 다소 과소 예측됨.
  • 입경이 클수록 수치 모델과 실험 모델 간 오차가 감소하는 경향을 보임(3mm 입경에서 보다 정확한 결과 도출됨).

향후 연구 방향

  • 다양한 유입 조건 및 퇴적물 특성에 따른 추가 시뮬레이션 수행.
  • LES(Large Eddy Simulation) 모델과 비교 연구 필요.
  • 실제 현장 데이터를 기반으로 모델 검증 연구 수행.

5. 연구의 의의

본 연구는 FLOW-3D를 활용하여 침수된 수평 제트로 인해 발생하는 국부 세굴 특성을 정량적으로 분석하고, 실험 데이터와 비교하여 모델의 신뢰성을 검증하였다. 이를 통해 수리 구조물 설계 시 세굴 방지 대책 수립에 기여할 수 있는 실질적인 데이터 및 분석 방법을 제공한다.

Fig. 1. A view of experimental flume model (Hosseini, 2008)
Fig. 1. A view of experimental flume model (Hosseini, 2008)
Fig. 3. A Plan of 2D graphical output of scour simulation results in Flow-3D numerical model
Fig. 3. A Plan of 2D graphical output of scour simulation results in Flow-3D numerical model

6. 참고 문헌

  1. Abdelaziz, S., M.D. Bui, P. Rutschmann, 2010. Numerical simulation of scour development due to submerged horizontal jet. River Flow. Process of the International Conference on Fluvial Hydraulics, 8–10 September, Braunschweig, Germany.
  2. Ali Hosseini, P., 2008. The study of local scour due to submerged horizontal Jets using experimental models. M.Sc. Thesis, University of Tehran, Tehran, Iran.
  3. Amir Aslani, Sh., M. Pirestani, A.A. Salehi neishabouri, 2008. Numerical study on the effects of internal friction angle of sediments on scour hole caused by free fall Jet. 2nd National Conference on Dam and Hydroelectric Power Plants, 14&15 May, Tehran, Iran.
  4. Bakhiet, Sh., G.A. Abdel-Rahim, K.A. Ali, N. Izumi, 2013. Prediction of scour downstream regulators using ANNs. International Journal of Hydraulic Engineering, 2; 1-13.
  5. Baranya S., J. Jozsa, 2006. Flow analysis in river Danube by field measurement and 3D CFD turbulence modelling. Journal of Periodica Polytechnica. Civil Engineering, 50; 57–68.
  6. Chatterjee, S., S. Ghoch, 1980. Submerged horizontal jet over erodible bed, Journal of the Hydraulics Division Proceedings of the American Society of Civil Engineers, 106; 1765-1782.
  7. Day, S., A. Sarkar, 2008. Characteristics of turbulent flow in submerged jumps on rough beds. Journal of Engineering Mechanic, 134; 49-59.
  8. Hager, W., H. Hans Erivin Minor, 2005. Plunge pool in prototype and laboratory. Hydraulics of Dam and River structures, London, 165-172.
  9. Hussein H.H, A.k.J. Inam, I.H. Nashwan, 2012. Evaluation of the local scour downstream untraditional bridge piers. Journal of Engineering and Development, 16; 36 – 49.
  10. Hamidifar, H., M.H. Omid, M. Nasrabadi, 2011. Scour downstream of a rough rigid apron. World Applied Sciences Journal 14; 1169-1178.
  11. Hopfinger, E.J., A. Kurniawan, W.H. Graf, W.U. Lemmin, 2004. Sediment erosion by Görtler vortices: The scour-hole problem. Journal of Fluid Mechanics, 520; 327-342.
  12. Karim, O.A., K.H.M. Ali, 2000. Prediction of patterns in local scour holes caused by turbulent water jets. Journal of Hydraulic Research, 38; 279-287.
  13. Khosronejad, A., S. Kang, F. Sotiropoulos, 2012. Experimental and computational investigation of local scour around bridge piers. Journal of Advances in Water Resources, 37; 73-85.
  14. Liu, X., M. García, 2008. Three-dimensional numerical model with free water surface and mesh deformation for local sediment scour. Journal of Waterway, Port, Coastal, and Ocean Engineering, ASCE, 134; 203–217.
Van Rijn Model

Flow-3D를 사용한 삼각형 래버린스 위어 하류의 하상 세굴에 대한 수치 시뮬레이션

본 소개 내용은 [Iranian Journal of Irrigation and Water Engineering]에서 발행한 [“Numerical Simulation of the Bed Scouring Downstream Triangular Labyrinth Weirs Using Flow-3D”] 의 연구 내용입니다.

Myer-Peter-Muller Model
Myer-Peter-Muller Model

서론

  • 연구 배경 및 필요성
    • 선형 위어에 비해 래버린스 위어는 폭 증가를 통해 흐름 용량을 증가시켜 특별한 관심을 받아왔음.
    • 위어 하류의 세굴 및 침식은 구조물 보호를 위해 중요하며, 위어 통과 유량 증가로 인해 하류 세굴량도 증가함.
    • 본 연구는 삼각형 평면을 가진 래버린스 위어의 수치 모델을 연구함.
  • 연구 목표
    • 다양한 요인(댐 본체 높이, 위어 정점 높이, 위어 통과 유량, 위어 정점 각도)이 래버린스 위어 하류의 하상 침식량에 미치는 영향을 연구하기 위해 23개의 모델을 Flow-3D 소프트웨어를 사용하여 시뮬레이션함.
    • 수치 시뮬레이션 결과와 실험 모델 결과의 검증을 통해 수치 시뮬레이션과 실험값 간의 매우 우수한 일치를 확인함.

연구 방법

  • 연구 설계
    • 3가지 정점 각도를 가진 삼각형 래버린스 위어 하류의 하상 세굴을 연구함.
    • 길이 10m, 폭 50cm, 높이 80cm의 인공 소형 수로에서 수치 모델을 수행함.
    • 4가지 위어 정점 각도(90°, 60°, 45°)를 테스트함.
  • 수치 모델링
    • 수로의 물 흐름과 상단의 공기 영역을 포함하는 다상 계산 영역을 다상 흐름 모델로 시뮬레이션함.
    • 계산 영역 준비 시 적절한 메시 생성은 매우 중요하며, 셀 크기가 세굴에 미치는 영향을 조사하기 위해 3가지 다른 셀 수를 적용함.
    • FLOW-3D는 광범위한 산업 응용 분야 및 물리적 프로세스에서 액체 및 기체의 동적 거동을 연구하는 엔지니어를 위한 완벽하고 다재다능한 CFD 시뮬레이션 플랫폼을 제공함.

연구 결과

  • 세굴 매개변수
    • 다양한 흐름 조건에서 래버린스 위어 하류의 최대 세굴 깊이, 최대 세굴 길이, 최대 퇴적 깊이 및 최대 퇴적 길이를 조사하기 위해 수치 시뮬레이션을 수행함.
    • 세굴 매개변수를 최소화하는 최적의 정점 각도를 찾기 위해 3가지 다른 위어 정점 각도(90°, 60°, 45°)에 대해 모델을 실행함.
    • 선형 위어 정점에 대한 최대 세굴 매개변수도 측정하여 비교함.
  • 결과 분석
    • 제시된 정점 각도로 삼각형 래버린스 위어를 사용하면 모든 세굴 및 퇴적 현상이 선형 위어에 비해 감소함.
    • 시뮬레이션 결과, 60°의 위어 정점 각도가 모든 세굴 및 퇴적 매개변수에서 더 큰 감소를 나타냄.
    • 선형 위어에 비해 상대 세굴 깊이, 세굴 길이, 퇴적 깊이 및 퇴적 길이에서 각각 약 89%, 77%, 45% 및 49% 감소가 관찰됨.

결론

  • 연구의 의의
    • 시뮬레이션 결과는 세굴 현상을 감소시키는 매우 효율적인 수단으로서 삼각형 래버린스 위어의 신뢰성을 나타냄.
    • 모든 위어 정점 각도에서 다양한 세굴 및 퇴적 매개변수의 감소가 관찰됨.
  • 최적의 위어 설계
    • 선형 위어에 비해 60°의 위어 정점 각도에서 더 낮은 세굴 매개변수가 획득됨.
    • 결론적으로, 최적의 위어 정점 각도인 60°는 선형 위어에 비해 세굴 매개변수를 최소화하고 에너지 소산을 최대화하는 잠재력을 가짐.
    • 세굴 지도는 대칭이며, 최대 세굴은 이동상 하상의 세로 중심선 좌우에서 발생함.
Van Rijn Model
Van Rijn Model
Myer-Peter-Muller Model
Myer-Peter-Muller Model

Reference

  1. D’Agostino, V. and Ferro, V. 2004. “Scour on alluvial bed downstream of grade-control structures.” Journal of Hydraulic Engineering, ASCE, 130(1): 24–37.
  2. Dargahi, B. (2003). “Scour development downstream of a spillway.” Journal of Hydraulic Research, 41(4): 417–426.
  3. Dey, S., Bose, S.K. and Sastry, G.L.N. 1995. “Clear-water scour at circular piers: a model.” Journal of Hydraulic Engineering, ASCE, 121(12): 869-876.
  4. Elnikhely, E.A. 2016. “Minimizing scour downstream of spillways using curved vertical sill.” Nineteenth International Water Technology Conference.
  5. Ettema, R. 1980. “Scour at bridge piers.” PhD Thesis, Auckland University, Auckland, New Zealand.
  6. Falvey, H.T. 2003. “Hydraulic design of labyrinth weirs.” ASCE Press, Reston, VA, United States.
  7. Flow Science, Inc. 2008. “FLOW-3D User’s Manual.” Flow Science, Inc.
  8. Gentilini, B. 1940. “Stramazzi con cresta a planta obliqua e a zig-zag, Memorie e Studi dell Instituto di Idraulica e Construzioni Idrauliche del Regil Politecnico di Milano, Italian.”
  9. Ghodsian, M. 2009. “Stage–discharge relationship for a triangular labyrinth spillway, in Proceedings of the Institution of Civil Engineers.” Water Management, 162(3): 173-178.
  10. Gupta, K.K., Kumar, S. and Ahmad, Z. 2015. “Effect of weir height on flow performance of sharp crested rectangular – planform weir.” World Applied Sciences Journal, 33(1): 168-175.
  11. Guven, A. and Gunal, M. 2008. “Prediction of scour downstream of grade-control structures using neural networks.” Journal of Hydraulic Engineering, ASCE, 134(11): 1656–1660.
  12. Heidarpour, M., Mousavi, S.F. and Roshanimehr, A.R. 2007. “Investigation of polyhedron weirs with rectangular plan and U-shaped, (in Persian).” Journal of Science and Technology of Agriculture and Natural Resources, 3(A): 1-11.
  13. Jüstrich, S., Pfister, M. and Schleiss, A.J. 2016. “Mobile riverbed scours downstream of a Piano Key weir.” Journal of Hydraulic Engineering, 142(11): 40-46.
  14. Kardan, N., Hakimzadeh, H. and Hassanzadeh, Y. (2013). “3D Numerical simulation of hydrodynamic parameters around the bridge piers using various turbulence models.” Journal of Irrigation Science and Engineering, 37(4): 39-54 (in Persian).
  15. Kumar, V., Rang Raju, K.G. and Vittal, N. 1999. “Reduction of local scour around bridge piers using slot and collars.” Journal of Hydraulic Engineering, ASCE, 125(12): 1302-1305.
  16. Kumar, B. and Ahmad, Z. 2020. “Experimental study on scour downstream of a piano key weir with nose.” 8th IAHR ISHS, Santiago, Chile.
  17. Melville, B.W. and Chiew, Y.M. 1999. “Time scale for local scour at bridge piers.” Journal of Hydraulic Engineering, ASCE, 125(1): 59-65.
  18. Melville, B.W. and Lim, S.Y. 2013. “Scour caused by 2D horizontal jet.” Journal of Hydraulic Engineering, 140(2): 149-155.
  19. Melville, B.W. 2015. “Scour at various hydraulic structures: sluice gates, submerged bridges and low weirs.” Conference: 5th IAHR International Symposium on Hydraulic Structures, Brisbane, Australia, 2014, Conference Paper, Australasian. Journal of Water Resources, 18(2): 101–117.
  20. Morsali M. 2019. “Investigation on scour downstream of triangular labyrinth weir.” M.Sc. thesis, University of Zanjan, Zanjan, Iran.
  21. Novak, P.J. 1961. “Influence of bed load passage on scour and turbulence downstream of stilling basin, in: 9th Congress, IAHR, Dubrovnik, Croatia.”
  22. Saleh, O.K., Elnikhely, E.A. and Ismail, F. 2019. “Minimizing the hydraulic side effects of weirs construction by using labyrinth weirs.” Flow Measurement and Instrumentation, 66: 1–11.
  23. Scurlock, S.M., Thornton, L.C. and Abt, S.R. 2012. “Equilibrium scours downstream of three-dimensional grade control structure.” Journal of Hydraulic Engineering, 138(2): 167-176.
  24. Schoklitsch Kolkbildungunteru, A. 1932. “Berfallstrahlen, Scour formation below overfall jets, Dieasserwirtschaft,” 25(24): 341–343 (in German).
  25. Sheppard, D.M. and Miller, W. 2006. “Live Bed Local pier scour experiments.” Journal of Hydraulic Engineering, ASCE, 132(7): 635-642.
  26. Smith, H. and Foster, D. 2005. “Modeling of flow around a cylinder over a scoured Bed.” Journal of Waterway, Port, Coastal, and Ocean Engineering, 14(1): 121-137.
  27. Van Rijn, L.C. 1984. “Principles of sediment transport in rivers, estuaries and coastal seas.” University of Utrecht, the Netherlands.
  28. Yazdi, A.M., Hoseini, S.A., Nazari, S. and Amanian, N. 2021. “Effects of weir geometry on scour development in the downstream of Piano Key Weirs.” Water Supply, 21(1): 289-298.
Figure 2. (a) Longitudinal depth averaged velocity contours and (b) velocity vectors' alignment around the cylindrical pier after 600 sec. of simulation with Flow-3D software

The Scour Bridge Simulation around a Cylindrical Pier Using Flow-3D

FLOW-3D를 이용한 원형 교각 주변의 세굴 시뮬레이션

Figure 2. (a) Longitudinal depth averaged velocity contours and (b) velocity vectors' alignment around the cylindrical pier
after 600 sec. of simulation with Flow-3D software
Figure 2. (a) Longitudinal depth averaged velocity contours and (b) velocity vectors’ alignment around the cylindrical pier after 600 sec. of simulation with Flow-3D software

연구 배경 및 목적

문제 정의

  • 교각 주변에서 발생하는 국부 세굴(local scour)은 유속 증가, 난류, 침식 작용에 의해 발생하며, 이는 교량 붕괴의 주요 원인 중 하나임.
  • 기후 변화로 인해 홍수 빈도가 증가하면서 교량 안전성 확보가 더욱 중요해짐.
  • 기존 실험 방식은 비용이 높고 유지보수가 어렵기 때문에 컴퓨터 기반 CFD 시뮬레이션을 활용한 예측 연구 필요.

연구 목적

  • FLOW-3D를 사용하여 원형 교각 주변에서 발생하는 국부 세굴을 시뮬레이션하고, 실험 데이터와 비교하여 모델의 신뢰성을 검증.
  • 유입 유량(5, 10, 19, 30 L/sec)에 따른 세굴 깊이 변화 분석.
  • 세굴 발생 위치와 유동 특성을 평가하여 교량 설계 및 유지보수에 활용할 데이터 제공.

연구 방법

시뮬레이션 모델링 및 설정

  • 수치 모델:
    • 채널 크기: 너비 0.4m, 길이 1.0m
    • 교각 크기: 지름 0.03m, 높이 0.3m
    • 퇴적층 크기: 길이 1.0m, 너비 0.4m, 높이 0.12m
  • 유체 해석 기법:
    • VOF(Volume of Fluid) 방법을 사용하여 유체-퇴적층 경계 추적
    • RNG k-ε 난류 모델을 적용하여 난류 흐름 해석
    • 침식 및 퇴적 모델: 입자 크기 0.72mm, 밀도 2650kg/m³, Shields 수 0.031 적용
  • 경계 조건:
    • 유입: 부피 유량 조건 적용
    • 유출: 출구 경계 조건 설정
    • 하부: 고정 벽 경계 적용
    • 상부: 대칭 경계 조건 사용

주요 결과

세굴 깊이 분석

  • 시뮬레이션 600초 후, 각 유량에서 최대 세굴 깊이:
    • 5 L/sec → 0.0cm
    • 10 L/sec → 1.3cm
    • 19 L/sec → 2.4cm
    • 30 L/sec → 3.6cm
  • 세굴 발생 패턴:
    • 교각 상류에서 세굴이 심하게 발생, 하류에서는 상대적으로 적음.
    • 말굽 와류(horseshoe vortex)와 수직 와류(vertical wake vortex)가 퇴적물 이동의 주요 원인임.

실험 데이터와 비교

  • 실험 결과와 비교 시, FLOW-3D 시뮬레이션은 상류에서 30%, 하류에서 20% 낮게 예측됨.
  • 이는 침식 역학에 대한 추가적인 보정이 필요함을 의미.
  • 하지만 전체적인 세굴 패턴 및 경향은 실험 결과와 일치.

결론 및 향후 연구

결론

  • FLOW-3D를 활용한 세굴 시뮬레이션이 실험 데이터와 높은 상관관계를 가짐을 확인.
  • 세굴 깊이는 유입 유량에 따라 증가하며, 상류에서 더 깊은 침식 발생.
  • 모델의 한계점(세굴 깊이 과소 예측)을 개선하기 위해 추가적인 침식 보정이 필요.

향후 연구 방향

  • 더 긴 시뮬레이션 시간 설정을 통한 침식-퇴적 균형 분석.
  • 다양한 교각 형상 및 하상 조건에서 추가 검증 수행.
  • 현장 측정 데이터와 비교하여 모델 신뢰성 향상.

연구의 의의

본 연구는 FLOW-3D를 활용하여 교각 주변 세굴을 시뮬레이션하고, 유량에 따른 세굴 패턴을 정량적으로 분석하였다. 이 결과는 향후 교량 설계 및 유지보수 전략 수립에 활용될 수 있으며, 홍수 시 교량 붕괴를 예방하는 데 기여할 것으로 기대된다.

Figure 1. Geometry and meshing structure of the model for simulation of scour around a cylindrical pier
Figure 1. Geometry and meshing structure of the model for simulation of scour around a cylindrical pier
Figure 2. (a) Longitudinal depth averaged velocity contours and (b) velocity vectors' alignment around the cylindrical pier
after 600 sec. of simulation with Flow-3D software
Figure 2. (a) Longitudinal depth averaged velocity contours and (b) velocity vectors’ alignment around the cylindrical pier after 600 sec. of simulation with Flow-3D software

References

  1. Abdelaziz, S., Bui, M.D., Rutschmann, P. 2010. Numerical simulation of scour development due to submerged horizontal jet, 5th River Flow, International Conference on Fluvial Hydraulics.
  2. Alabi, P.D. 2006. Time development of local scour at bridge pier fitted with a collar. Master Science Thesis, University of Saskatchewan, Canada.
  3. Briaud, J.L., Gardoni, P., Yao, C. 2012. Bridge Scour Risk, ICSE6 Paris. ICSE6-011.
  4. Elsebaie, I.H. 2013. An Experimental Study of Local Scour around Circular Bridge Pier in Sand Soil, International Journal of Civil & Environmental Engineering (IJCEE-IJENS), 13(1), 23-28.
  5. Flow-3D v.9.2, Flow Science Inc., 2007, User’s Manual. www.flow3d.com.
  6. Jafari, M., Ayyoubzadeh, S.A., Esmaeili Varaki, M., Rostami, M. 2017. Simulation of Flow Pattern around Inclined Bridge Group Pier using FLOW-3D Software. Journal of Water and Soil, 30(6), 1860-1873.
  7. Heidarpour, M., Afzalimehr, H., Izadinia, E. 2010. Reduction of local scour around bridge pier groups using collars, International Journal of Sediment Research, 25(4): 411-422.
  8. Melville, B.W., Sutherland. A.J. 1988. Design method for local scour at bridge piers. J. Hyd. Eng, 114(10): 1210-1226.
  9. Olsen, N.R. 2007. A three dimensional numerical model for simulation of sediment movements in water intakes with multiblock option, User’s manual [Online]. Available: http://www.ntnu.no.
  10. Prendergast L.J., Gavin, K. 2014. A review of bridge scour monitoring techniques, Journal of Rock Mechanics and Geotechnical Engineering, 6, 138-149.
  11. Ramezani, Y., Babagoli Sefidkoohi, R. 2016. Comparison of Turbulence Models for Estimation of Bed Shear Stress Around Bridge Abutment in Compound Channel, Water and soil science, 26(2): 95-109.
  12. Soltani-Gerdefaramarzi, S., Afzalimehr, H., Chiew, Y.M., Lai, J.S. 2013a. Jets to control scour around circular bridge piers. Canadian journal of civil engineering, 40(3), 204-212.
  13. Soltani-Gerdefaramarzi, S., Afzalimehr, H., Chiew, Y.M., Ghasemi, M. 2013b. Turbulent characteristics in flow subjected to bed suction and jet injection as a pier-scour countermeasure, International Journal of Hydraulic Engineering, 2(5), 93-100.
  14. Soltani-Gerdefaramarzi, S., Afzalimehr, H., Chiew, Y.M., Gallichand, J. 2014. Reduction of pier scour using bed suction and jet injection. Water management. 167(2), 105-114.
  15. Smith, H. 2007. Flow and sediment dynamics around three-dimensional structures in coastal environments, Ph.D. thesis, The Ohio State University.
  16. Yildiz, B., Koken, M., Gogus, M. 2013. Abutment Scour Simulations by Using FLOW-3D, FLOW-3D user conference, Flow Science Inc.
Fig. 8 Computation of (TKE) in horizontal sections of basin at end time of simulation

The Numerical Investigation on Vortex Flow Behavior Using FLOW-3D

FLOW-3D를 이용한 와류 유동 거동에 대한 수치적 연구

1. 서론

  • 와류 침전지(Vortex Settling Basin, VSB)는 유동의 와류 현상을 이용하여 침전물을 분리하는 장치로, 기존 침전지보다 비용이 적게 들고 공간 활용도가 높음.
  • VSB 내의 유동은 강제 와류(Forced Vortex)와 자유 와류(Free Vortex)로 구성되며, 이들의 형성과 거동을 정확히 이해하는 것이 중요함.
  • 본 연구는 FLOW-3D를 이용하여 와류 침전지 내부의 3차원 난류 유동을 수치적으로 분석하고, 실험 데이터를 통해 모델의 신뢰성을 검증하는 것을 목표로 함.

2. 연구 방법

실험 및 수치 모델 개요

  • 실험 장치
    • 직경 0.7m, 깊이 1.5m의 원형 와류 침전지 사용.
    • 중앙 배출구(Flush Pipe) 직경: 0.075m.
    • 입구 및 배출구 배치는 Paul et al.(1991)의 설계 권장사항을 따름.
  • FLOW-3D 기반 CFD 시뮬레이션 설정
    • VOF(Volume of Fluid) 기법을 사용하여 자유 수면 추적.
    • RNG k-ε 난류 모델을 적용하여 난류 해석 수행.
    • 격자(Grid) 설정: 중심부 0.5cm, 벽면 주변 1cm, 나머지 영역 2cm.
    • 경계 조건:
      • 유입: 부피 유량 조건(volume flow rate).
      • 유출: 자유 배출(outflow) 경계 조건.
      • 벽면: No-slip 조건 적용.

3. 연구 결과

유동 패턴 및 와류 형성

  • 강제 와류와 자유 와류가 동시에 존재하며, 시간이 지나면서 와류 강도가 변화함.
  • 중앙부에서 강한 와류 코어 형성 후, Overflow Jet에 의해 변형되는 현상 확인.
  • 와류 중심(Core)이 초기에는 유지되다가 시간이 지나면서 점차 소멸되는 현상 관찰.

난류 강도 및 에너지 해석

  • 침전지 중앙부에서 난류 강도가 가장 높고, 벽면에서는 상대적으로 낮음.
  • 시간이 경과할수록 에너지가 감소하며, Overflow Jet이 난류 강도를 증가시키는 역할을 함.
  • 실험 결과와 비교했을 때, 수치 모델이 높은 정확도를 보이며, 최대 5% 이내의 오차율 확인.

4. 결론 및 제안

결론

  • FLOW-3D 기반 시뮬레이션이 실험 결과와 높은 신뢰도로 일치하며, 와류 침전지의 유동 거동을 정밀하게 분석할 수 있음.
  • 중앙부에서 형성된 강한 와류가 시간이 지남에 따라 소멸되며, Overflow Jet이 유동 패턴을 크게 변화시킴.
  • 기존 이론 모델(Rankine Combined Vortex)과 비교 시, 실제 유동에서는 난류 효과로 인해 와류 코어가 변형됨.

향후 연구 방향

  • 다양한 입구 및 배출구 배치 조건에서의 추가 실험 및 시뮬레이션 수행.
  • LES(Large Eddy Simulation) 모델과의 비교 연구.
  • 실제 현장 데이터를 활용한 검증 연구 진행.

5. 연구의 의의

본 연구는 FLOW-3D를 활용하여 와류 침전지의 유동 및 난류 특성을 정량적으로 분석하고, 실험 데이터를 통해 모델의 신뢰성을 검증하였다. 수처리 시스템 및 하천 공학 분야에서 VSB 설계 최적화에 기여할 수 있는 데이터 및 분석 방법을 제공한다.

6. 참고 문헌

  1. Paul, T.C., S.K. Sayal, V.S. Sakhanja and G.S. Dhillon, 1991. Vortex settling chamber design considerations. J. Hyd. Engng., 117(2): 172-189.
  2. Mashauri, D.A., 1986. Modeling of vortex settling chamber for primary clarification of water. PhD thesis, Tampere University of Technology, Tampere, Finland, pp: 217.
  3. Salakhov, F.S., 1975. Rotational design and methods of hydraulic calculation of load-controlling water intake structures for Mountain Rivers. Proceedings of Ninth Congress of the ICID, Moscow, Soviet Union, pp: 151-161.
  4. Cecen, K., 1977. Hydraulic criteria of settling basins for water treatment, hydro-power and irrigation. Proc. 17th Congress of the Int. Assoc, of Hydr. Res., BadenBaden, West Germany, pp: 275-294.
  5. Cecen, K. and N. Akmandor, 1973. Circular settling basins with horizontal floor. MAG Report No 183, TETAK, Ankara, Turkey.
  6. Cecen, K. and M. Bayazit, 1975. Some laboratory studies of sediment controlling structures calculation of load-controlling water intake structures for Mountain Rivers. Proceedings of the Ninth Congress of the ICID, Moscow, Soviet Union, pp: 107-110.
  7. Mashauri, D.A., 1986. Modeling of vortex settling chamber for primary clarification of water, PhD thesis, Tampere University of Technology, Tampere, Finland, pp: 217.
  8. Anwar, H.O., 1969. Turbulent flow in a vortex. J. Hydr. Res., 7(1): 1-29.
  9. http://www.flow3d.com/resources/flow3d-technical-papers-1.html.
  10. Chapokpour, J. and J. Farhoudi, 2011. Sediment extraction and flow structure of vortex settling basin. WASJ., 14(5): 782-793.
  11. Isfahani, A.H.G. and J.M. Brethour, 2009. On the Implementation of Two-equation Turbulence Models in FLOW-3D, Flow Science, FSI-09-TN86.
Fig. 8. Three-dimensional modeling of a serrated stepped spillway

Numerical Study of Energy Dissipation in Baffled Stepped Spillway Using Flow-3D

FLOW-3D를 이용한 배플형 계단식 여수로의 에너지 소산에 대한 수치 연구

1. 서론

  • 댐 건설은 효율적인 저수지 조성, 저장 및 최적 활용을 목표로 하며, 이에 따라 수리학적 설계가 중요함.
  • 여수로(spillway)는 댐의 보조 구조물로서 초과 유량을 안전하게 하류로 방출하는 역할을 수행하며, 이 과정에서 잠재적 에너지를 운동 에너지로 변환하여 하류부 침식을 초래할 수 있음.
  • 계단식 여수로(stepped spillway)는 유입 공기를 증가시키고 흐름 속도를 줄여 운동 에너지 소산을 향상시키는 효과가 있음.
  • 본 연구는 FLOW-3D를 이용한 배플형 계단식 여수로의 유동 및 에너지 소산 특성을 수치적으로 분석하고, 실험 결과와 비교하여 신뢰성을 평가하는 것을 목표로 함.

2. 실험 모델

  • 실험 장치 개요:
    • 계단식 여수로 모델과 모래 바닥을 포함한 수조로 구성.
    • 다양한 유량과 경사 조건에서 실험 수행.
    • 배플 블록(Block A~E)은 거친 표면을 가지며, 인접한 블록과 90° 회전된 형태로 배치됨.
  • 기존 연구(Kamyab Moghaddam et al.)에서 사용된 실험 방법론을 적용하여 모델 검증 수행.

3. 수치 모델링

  • FLOW-3D 모델 설정:
    • VOF(Volume of Fluid) 기법을 사용하여 자유 수면 추적.
    • RNG k-ε 난류 모델을 적용하여 난류 해석 수행.
    • FAVOR(Fractional Area/Volume Obstacle Representation) 기법을 적용하여 복잡한 형상을 해석 가능하게 함.
  • 경계 조건 설정:
    • 유입부(X min): 부피 유량 조건(Volume flow rate) 적용.
    • 유출부(X max): 자유 배출(Outflow) 경계 조건 설정.
    • 벽면(Y min, Y max): 대칭 경계 조건(Symmetry) 적용.
    • 상단(Z max) 및 바닥(Z min): 각각 자유 수면 및 고체 경계 설정.

4. 모델링 결과

  • FLOW-3D 시뮬레이션과 실험 비교 결과:
    • 평균 제곱근 오차(RMSE) = 0.02, 즉 실험 결과와 매우 높은 일치도 확인.
    • 배플 블록이 유동 난류를 증가시켜 전체 에너지의 77%를 소산하는 것으로 나타남.
  • 상대적 에너지 소산율(∆E/E₀) 분석:
    • 유량이 증가할수록 에너지 소산율은 감소하지만, 배플 블록이 없는 경우보다 높은 소산 효과 유지.
    • 실험 및 수치 해석 결과의 에너지 소산율 차이는 최대 2% 이내로 매우 낮음.

5. 결론 및 제안

결론

  • 배플형 계단식 여수로는 기존 계단식 여수로보다 높은 에너지 소산 효과를 가짐.
  • FLOW-3D 기반 시뮬레이션이 실험 데이터와 높은 신뢰도로 일치하며, 수리학적 거동 분석에 효과적임.
  • 배플 블록의 배열과 형상이 유동 난류 및 에너지 소산에 중요한 영향을 미침.

향후 연구 방향

  • 장기적인 캐비테이션(cavitation) 및 구조적 안전성 분석 필요.
  • 실제 현장 데이터를 기반으로 추가적인 최적 설계 연구 진행.
  • 다양한 배플 블록 형상 및 배치 조건에서의 추가 실험 수행.

6. 연구의 의의

본 연구는 FLOW-3D를 활용하여 배플형 계단식 여수로의 유동 및 에너지 소산 특성을 정량적으로 분석하고, 수치 모델의 신뢰성을 실험적으로 검증하였다. 향후 여수로 설계 최적화 및 홍수 방지 인프라 구축에 기여할 수 있는 데이터 및 분석 방법을 제공한다.

7. 참고 문헌

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Graphical Abstract

Flow-3D Numerical Modeling of Converged Side Weir

수렴형 측방 위어의 FLOW-3D 수치 모델링

연구 배경 및 목적

문제 정의

  • 측방 위어(side weir)는 수로 및 하천에서 홍수 조절, 유량 분배 및 관개 시스템에서 중요한 역할을 함.
  • 기존 연구는 주로 단순한 프리즘형(prismatic) 채널에서 수행되었으며, 수렴형(converged) 채널에서의 측방 위어 성능 연구는 부족함.
  • 수렴형 채널에서 위어의 효율성 증대 가능성을 검토하고, FLOW-3D를 이용한 정량적 분석이 필요함.

연구 목적

  • FLOW-3D를 사용하여 수렴형 채널에서 측방 위어의 유동 특성을 수치적으로 분석.
  • 실험 모델과 비교하여 FLOW-3D의 신뢰성을 검증.
  • 수렴각 및 하류 채널 폭 변화가 위어 성능(유량 분배, 수위 변화, 에너지 손실 등)에 미치는 영향 평가.

연구 방법

실험 및 수치 모델 개요

  • 실험 환경:
    • 실험실 규모 수로(길이 700mm, 폭 310mm, 높이 480mm).
    • 다양한 위어 길이(5개), 위어 크레스트 높이(4개), 수렴각(2개), 하류 채널 폭(3개) 조건에서 총 33개 실험 수행.
    • 유량 범위: 10~100m³/h.
  • FLOW-3D 기반 CFD 시뮬레이션 설정:
    • VOF(Volume of Fluid) 기법을 사용하여 자유 수면 추적.
    • RNG k-ε 난류 모델 적용.
    • 격자(Grid) 설정: 메쉬 크기 1cm, 전체 셀 수 모델 크기에 따라 조정.
    • 경계 조건:
      • 유입: 부피 유량 조건(volume flow rate).
      • 유출: 자유 배출(outflow) 경계 조건.
      • 벽면: No-slip 조건 적용.

주요 결과

수렴형 vs. 프리즘형 채널 비교

  • 수렴형 채널에서 하류 폭을 감소시키면 위어 상류 수심이 증가하여 위어를 통한 유량 분배 증가.
  • 수렴각이 클수록 수위 및 특정 에너지가 증가하여 유출량(Qw/Q0) 비율 향상.
  • 프리즘형 채널 대비 수렴형 채널이 동일한 유량에서도 더 높은 위어 크레스트 수위를 형성하여 방류 효율성이 증가.

수위 및 유속 분포 분석

  • 위어 상류 및 중간부에서 수면 경사가 하강하는 경향, 그러나 위어 끝에서는 상승하는 패턴 확인.
  • 최대 유속이 수렴 채널에서 위어 시작점 근처에서 발생, 반면 횡방향 유속은 위어 중앙부에서 최대값 도달.
  • 에너지 손실 분석 결과, 하류 채널 폭 감소(b/B ↓)에 따라 에너지 손실 감소, 이는 유량 분배 효율 증가로 연결됨.

결론 및 향후 연구

결론

  • FLOW-3D 시뮬레이션 결과와 실험 데이터가 높은 일치도를 보이며(R² = 0.98), 수렴형 측방 위어의 유동 특성을 효과적으로 예측 가능.
  • 수렴형 채널에서 위어의 효율성이 증가하며, 하류 채널 폭이 줄어들수록 위어 상류 수위가 상승하여 방류량이 증가.
  • b/B 비율이 작을수록(즉, 하류 채널이 좁을수록) 위어의 성능이 개선됨.

향후 연구 방향

  • LES(Large Eddy Simulation) 모델과의 비교 분석 수행.
  • 다양한 채널 형상 및 유량 조건에서 추가적인 검증 수행.
  • 실제 하천 및 관개 시스템 적용을 위한 최적 설계 모델 연구.

연구의 의의

이 연구는 FLOW-3D를 활용하여 수렴형 측방 위어의 유동 및 에너지 특성을 분석하고, 실험 데이터를 통해 모델의 신뢰성을 검증하였다. 수렴형 채널 설계를 통해 위어 성능을 최적화할 수 있음을 입증하며, 실무 적용 가능성이 높음.

References

  1. Abbasi S, Fatemi S, Ghaderi A, Di Francesco S (2021). “The Effect of Geometric Parameters of the Antivortex on a Triangular Labyrinth Side Weir.” Water, 13(1), 14. https://doi.org/10.3390/w13010014
  2. Ackers P (1957). “A Theoretical Consideration of Side-weirs as Storm Water Overflows.” Proceeding of Institute of Civil Engineers, 6, 250–269.
  3. Afshar H, Hoseini SH (2013). “Experimental and 3-D Numerical Simulation of Flow Over a Rectangular Broad-Crested Weir.” International Journal of Engineering and Advanced Technology (IJEAT), 2(6), 214–219.
  4. Al-Hashimi AS, Madhloom MH, Nahi NT (2017). “Experimental and Numerical Simulation of Flow Over Broad Crested Weir and Stepped Weir Using Different Turbulence Models.” Journal of Engineering and Sustainable Development, 21(2), 28–45.
  5. Aydin MC (2012). “CFD Simulation of Free-Surface Flow Over Triangular Labyrinth Side Weir.” Adv Eng Softw, 45(1), 159–166. https://doi.org/10.1016/j.advengsoft.2011.09.006
  6. Azimi H, Shabanlou S, Ebtehaj I, Bonakdari H (2016). “Discharge Coefficient of Rectangular Side Weirs on Circular Channels.” International Journal of Nonlinear Sciences and Numerical Simulation, 17(7–8), 391–399. https://doi.org/10.1515/ijnsns-2016-0033
  7. Bagheri S, Heidarpour M (2011). “Characteristics of Flow Over Rectangular Sharp Crested Side Weirs.” J Irrig Drain Eng, 138(6), 541–547. https://doi.org/10.1061/(ASCE)IR.1943-4774.0000433
  8. Borghei SM, Parvaneh A (2011). “Discharge Characteristics of a Modified Oblique Side Weir in Subcritical Flow.” Flow Meas Instrum, 22(5), 370–376. https://doi.org/10.1016/j.flowmeasinstr.2011.04.009
  9. Granata F, Di Nunno F, Gargano R, de Marinis G (2019). “Equivalent Discharge Coefficient of Side Weirs in Circular Channel—A Lazy Machine Learning Approach.” Water, 11(11), 2406. https://doi.org/10.3390/w11112406
  10. Hager WH (1987). “Lateral Outflow Over Side Weirs.” J Hydraulic Engineering, 113(4), 491–504. https://doi.org/10.1061/(ASCE)07339429(1987)113:4(491)
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Figure 4 Simulated velocity magnitude

An Experimental and Numerical Study of Ski-Jump Spillway Using FLOW-3D

FLOW-3D를 이용한 스키점프형 여수로의 실험 및 수치적 연구

연구 배경 및 목적

문제 정의

  • 스키점프형 여수로는 유속이 20m/s를 초과할 때 사용되는 중요한 구조물이며, 에너지 소산을 위한 핵심 설계 요소임.
  • 기존의 물리 실험은 비용이 높고 시간이 많이 소요되므로 컴퓨터 기반 CFD(전산유체역학) 시뮬레이션을 통한 연구가 필요함.

연구 목적

  • FLOW-3D를 이용하여 스키점프형 여수로의 유동 특성을 수치적으로 분석.
  • 실험 데이터와 비교하여 FLOW-3D 모델의 정확성을 검증.
  • 여수로의 제트 궤적(jet trajectory), 압력 분포 및 에너지 소산 특성 분석.

연구 방법

실험 및 수치 모델 개요

  • 연구 대상: IS 7365 (2010) 표준을 따른 전통적인 스키점프형 여수로.
  • 실험 조건:
    • 수로 크기: 폭 0.30m, 깊이 0.30m, 길이 6m의 유리제 수리 실험 수로.
    • 연속된 곡면 립(lip) 각도 35°, 반경 0.0915m.
    • 유량(Q): 0.00431 ~ 0.00962 m³/s 범위.

FLOW-3D 기반 CFD 시뮬레이션 설정

  • VOF(Volume of Fluid) 기법을 사용하여 자유 수면 추적.
  • RNG k-ε 난류 모델을 적용하여 난류 해석 수행.
  • FAVOR(Fractional Area/Volume Obstacle Representation) 기법을 적용하여 장애물 영역 설정.
  • 경계 조건:
    • 유입: 지정 속도 조건.
    • 유출: 지정 압력 조건.
    • 벽면: No-slip 조건 적용.

주요 결과

유동 및 에너지 소산 특성 분석

  • 스키점프형 여수로에서 유동이 곡면을 따라 흐르면서 에너지가 점진적으로 소산됨.
  • FLOW-3D 결과와 실험 데이터의 에너지 소산율 비교
    • 최대 오차율 15.69%로 나타났으며, 실험과 높은 일치도를 보임.
    • 유량이 증가할수록 에너지 소산율이 감소하는 경향 확인.
  • 제트 궤적 및 압력 분포 분석
    • 시뮬레이션 결과와 실험값이 3D 유동장 및 압력 분포에서 일치함을 확인.

결론 및 향후 연구

결론

  • FLOW-3D 기반 시뮬레이션이 실험 결과와 높은 일치도를 보이며, 스키점프형 여수로의 유동 및 에너지 소산 특성을 효과적으로 예측 가능.
  • 유량 변화에 따른 에너지 소산율 감소 경향을 확인하였으며, 추가적인 최적화 연구 필요.

향후 연구 방향

  • LES(Large Eddy Simulation) 난류 모델과 비교 분석 수행.
  • 다양한 여수로 형상 및 유량 조건에서 추가적인 검증 수행.
  • 실제 댐 적용 사례와 비교 연구 수행.

연구의 의의

이 연구는 FLOW-3D를 활용하여 스키점프형 여수로의 유동 및 에너지 소산 현상을 정량적으로 분석하고, 수치 모델의 정확성을 실험적으로 검증하였다. 댐 설계 및 홍수 방지 인프라 구축에 중요한 데이터와 분석 방법을 제공한다.

References

  1. High Overflow Dams, Hydraulic Design Criteria, U.S. Army Corps of Engineers, Waterways Experiment Station, 1970.
  2. R. Maitre, S. Obolensky, Etude de Quelques Caractéristiques de l’Ecoulement dans la Partie Aval des Evacuateurs de Surface, La Houille Blanche 4 (1954) 481–511.
  3. T.J. Rhone, A. J. Peterka, Improved tunnel spillway flip buckets, Journal of Hydraulic Engineering, ASCE 126 (1959) 1270–1291.
  4. A.C. WATERS, Terraces and coulees along the Columbia River near lake Chelan, Washington. Geological Society of America Bulletin 44 (1933) 783–820.
  5. R. Joun, W.H. Hager, Flip bucket without and with deflectors, Journal of Hydraulic Engineering, ASCE 126 (2000) 837–845.
  6. M. Jorabloo, R. Maghsoodi, H. Sarkardeh, 3D Simulation of flow over flip buckets at dams, Journal of American Science 7 (2011) 931–936.
  7. O. A. Yamini, M. R. Kavianpour, Experimental study of static and dynamic pressures over simple flip bucket, 5th symposium on advances in science and technology, Khavaran Highereducation Institute, Mashhad, Iran. May 12-14 (2011).
  8. O.A. Yamini, M.R. Kavianpour, S.H. Mousavi, A. Movahedi, . Bavandpour, Experimental investigation of pressure fluctuation on the bed of compound flip buckets, ISH Journal of Hydraulic Engineering 1 (2017) 1–8.
  9. P. Novak, C. Nalluri, R. Narayanan, Hydraulic Structures, Forth Edition, Taylor & Francis, New York (2007) 246–265.
  10. M.H. Chaudhry, Open-Channel Flow, Second Edition, Springer, 2008.
  11. L. Schmocker, M. Pfister, W.H. Hager, H. E. Minor, Aeration characteristics of ski jump jets, Journal of Hydraulic Engineering, ASCE 134 (2008) 90–97.
  12. M. R. Bhajantri, T.I. Eldho, P.B. Deolalikar, Hydrodynamic modelling of flow over a spillway using a two-dimensional finite volume-based numerical model, Sadhana 31 (2006) 743–754.
  13. F.A. Bombardelli, I. Meireles, J. Matos, Laboratory measurements and multi-block numerical simulation of the mean flow and turbulence in the non-aerated skimming flow region of steep stepped spillways, Environ Fluid Mech, Springer 11 (2011) 263–288.
  14. P.G. Chanel, J.C. Doering, An evaluation of computational fluid dynamics for spillway modelling, 16th Australian Fluid Mechanics Conference, Crown Plaza, Gold Coast, Australia, (2007).
  15. B. M. Savage, and M. C. Johanson, Flow over ogee spillway: physical and numerical model case study, J. of Hydraulic Engineering, ASCE 127 (2001) 640–649.
  16. G. Heidarinejad, and A. Najibi, Two-dimensional analysis of flow at the toe of a dam, Proceedings of Intl. Conf. on Hydraulic Structures, Shahid Bahonar Kerman University, Kerman, (2001).
  17. D.K. Ho, H.K.M. Boyes, S.M. Donohoo, Investigation of spillway behaviour under increased maximum flood by computational fluid dynamics technique, 14th Australian Fluid Mechanics Conference, Adelaide University, Adelaide, Australia, (2001).
  18. S. Eklund, CFD modelling of ski-jump spillway in Stornnforsen, Master’s Thesis, Royal Institute of Technology, Sweden, (2017).
Velocity Magnitude

Study of Velocity, Flow Depth and Froude Number of HDPE Diagonal Modular Pavement Using FLOW-3D

FLOW-3D를 이용한 HDPE 대각선 모듈러 포장(HDP Diagonal Modular Pavement)의 속도, 유동 깊이 및 Froude 수 연구

연구 배경 및 목적

  • 문제 정의: 기존의 아스팔트 포장 도로물의 자연스러운 흐름을 방해하고 홍수 위험을 증가시키는 환경적 문제를 초래한다.
    • 모듈러 포장 시스템(Modular Pavement System)은 투수성 재료와 중첩된 빈 공간 구조를 통해 강우 유출을 줄이고 지하수 재충전을 촉진할 수 있다.
    • 그러나 물리적 실험 방법은 비용이 많이 들고 시간 소모적이기 때문에, 수치 시뮬레이션을 통한 효율적 설계 방법이 필요하다.
  • 연구 목적:
    • FLOW-3D 소프트웨어를 활용하여 대각선 HDPE 모듈러 포장 시스템의 수리적 특성(속도, 유동 깊이, Froude 수)을 분석.
    • 말레이시아 실제 강우 데이터를 사용하여 다양한 강우 강도(5 mm/h 및 85 mm/h)에 따른 포장의 물 흡수 능력 평가.
    • 예비 설계 방법으로서의 FLOW-3D 사용 가능성 검증.

연구 방법

  1. 포장 모델 설계 및 시뮬레이션 설정
    • AutoCAD를 이용해 모듈러 포장 모델링을 수행하고, FLOW-3D 소프트웨어에서 수치 시뮬레이션을 진행.
    • 포장 모델 구성:
      • 모듈러 포장층, 자갈층, 모래층의 3가지 레이어로 구성.
      • HDPE 모듈러 포장80 mm 직경, 5 mm 두께의 얇은 대각선 기둥 구조.
      • Jabatan Kerja Raya 표준에 따라 설계.
    • 수치 모델 설정:
      • FLOW-3D의 VOF(Volume of Fluid) 기법을 사용하여 유체 흐름 및 유동 깊이 예측.
      • Navier-Stokes 방정식을 사용하여 3차원 불압축성 유동(Incompressible Flow) 시뮬레이션.
      • 모듈러 포장 모델의 경계 조건대칭(Symmetry), 연속(Continuative), 체적 유량(Volume Flow Rate), 벽(Wall) 경계로 설정.
  2. 시뮬레이션 시나리오 및 변수 설정
    • 강우 강도 시나리오:
      • 낮은 강우(5 mm/h)높은 강우(85 mm/h) 조건을 설정하여 모듈러 포장의 유동 특성 분석.
    • 측정 변수:
      • 속도(속도의 x, y, z 성분), 유동 깊이(Flow Depth), Froude 수(Fr)를 측정.
      • Froude 유속과 관성력의 비율을 나타내며, 유동 상태(서브크리티컬 또는 슈퍼크리티컬) 평가에 사용.

주요 결과

  1. 속도(X-, Y-, Z-방향) 분석
    • 시뮬레이션 결과:
      • x, y 속도z 속도보다 크게 나타남.
      • 200초 초기 단계에서 x 속도는 122.40 ~ 125.28 cm/h, 6000초 후에는 68.04 ~ 78.12 cm/h로 감소.
      • z 속도는 40.68 ~ 44.28 cm/h(200초)에서 22.32 ~ 30.6 cm/h(6000초)로 다소 적은 변화를 보임.
    • 속도 감소 원인 분석:
      • 낮은 토양 투수성으로 인해 강우 강도가 유속에 미치는 영향 미미.
      • 모듈러 포장 구조 내 작은 기공(Pore Space)과 모세관 현상(Capillarity) 제한으로 유속 감소.
  2. 유동 깊이(Flow Depth) 변화 분석
    • 모든 강우 강도 조건(5 mm/h, 85 mm/h)에서 유동 깊이는 425.65 mm로 일정하게 유지.
    • 포장 내 물의 유입 및 유출이 균형을 이루어 정상 상태(Steady State) 도달.
    • 포장 구조의 투수성 덕분에 강우 강도가 증가해도 표면 유출(Surface Runoff)이 발생하지 않음.
  3. Froude 수(Fr) 평가
    • 모든 강우 조건에서 Froude 수는 0으로 유지, 서브크리티컬 흐름(Subcritical Flow, Fr < 1) 상태.
    • 모듈러 포장이 물 저장 및 투수 역할을 수행하여 흐름 에너지를 낮추고 난류(Turbulence) 감소 효과.
    • 높은 Froude 수낮은 전단력 방출(Shear Force Discharge) 및 높은 침전물 운반 용량을 의미하지만, 본 연구에서는 낮은 Fr 값으로 침전물 운반 감소 효과 확인.

결론 및 향후 연구

  • 결론:
    • FLOW-3D 소프트웨어를 활용하여 HDPE 모듈러 포장의 수리적 특성을 정확히 분석 가능.
    • 모듈러 포장이 강우 유출을 줄이고 지하수 충전에 효과적임을 입증.
    • 말레이시아 실제 강우 데이터를 활용하여 현지 조건에서도 적합성을 보임.
    • FLOW-3D는 모듈러 포장 설계 시 예비 평가 도구로 활용 가능.
  • 향후 연구 방향:
    • 다양한 경사(Slope) 조건에서의 모듈러 포장 성능 분석 필요.
    • 최적 강우 강도 및 침투 효율성 평가를 위한 시뮬레이션 확장.
    • AI 및 머신러닝을 활용한 실시간 수리적 성능 예측 모델 개발.

연구의 의의

이 연구는 FLOW-3D를 활용하여 HDPE 대각선 모듈러 포장의 수리적 성능을 정량적으로 평가하고, 비용 효율적인 강우 관리 및 침수 예방을 위한 설계 가이드라인을 제공하며, 도시 홍수 위험을 줄이고 지속 가능한 물 관리 정책 수립에 기여할 수 있다​.

Reference

  1. Vaitkus et al. 2021 Concrete Modular Pavement Structures with Optimized Thickess Based onCharacteristics of High Performance Concrete Mixtures with Fibers and Silica FumeMaterials 14 (3423) 1-17.
  2. Shafique, M., Kim, R., & Kwon, K. H. 2018 Rainfall Runoff Mitigation by Retrofitted PermeablePavement in an Urban Area Sustainability (Switzerland) 10 (4)
  3. Chen et al. 2020 Effect of Rainfall, Runoff and Infiltration Processes on the Stabily of FootslopesWater 12 (1229) 1-19.
  4. Ahn et al. 2018 Development of Test Equipment for Evaluating Hydraulic Conductivity ofPermeable Block Pavement Sustainability 10 (2549) 1-16.
  5. Rashid, M. A., Abustan, I., & Hamzah, M. O. 2012 Infiltration Characteristic Modeling UsingFlow3d within a Modular Pavement Procedia Engineering 50 (Icasce) 658–667.
  6. Sharma, S., Sharma, P. K., & Upadhyay, N. 2020 Properties of Bituminous Bindermodified withPolyethylene Journal of Physics: Conference Series 1531 (1).
  7. Jabatan Kerja Raya. 2013 Manual Pavement Design.qxd. 1–29.
  8. Li, Z., Sun, X., Wang, F., & Liang, Y. 2018 Microscopic Flow Characteristics of Fluids in PorousMedium and Its Relationship with Remaining Oil Distribution: A Case Study in SaertuOilfield of Daqing In China Geofluids 2018.
  9. Abdurrasheed et al. 2019 Modelling of Flow Parameters through Subsurface Drainage Modulesfor Application in BIOECODS Water (Switzerland) 11 (9) 1–15.
  10. Zhao et al (2019) Effects of Rainfall Intensity and Vegetation Cover on Erosion Characteristicsof a Soil Containing Rock Fragments Slope Advances in Civil Engineering 2019.
  11. Song et al. (2014) Study of The Fluid Flow Characteristics in a Porous Medium For CO2Geological Storage using MRI Magnetic Resonance Imaging 32 (5) 574–584.
  12. Payus et al. (2020) Impact of Extreme Drought Climate on Water Security in North Bornea: CaseStudy of Sabah Water 12 (1135) 1-19.
  13. Cherkauer, D. S. (2021). The effect of urbanization on kinetic energy distributions in smallwatersheds.
  14. Zhang et al (2015) Approximate Simulation of Strom Water Runoff over Pervious PavementInternational Journal of Pavement Engineering 18 (3) 247-259
  15. Liu et al. (2019) Laboratory Analysis on the Surface Runoff Pollution Reduction Performance ofPermeable Pavements Science of the Total Environment 691 1–8.
  16. Khan et al. (2016) Effect of Slope, Rainfall Intensity and Mulch on Erosion and Infiltrationunder Simulated Rain on Purple Soil of South-Western Sichuan Province, China Water(Switzerland) 8 (11) 1–18.
  17. Lee et al (2013) Modelling the Hydrologic Process of a Permeable Pavement System Journal ofHydrologic Engineering 20 (5) 04014070
  18. Wolff, A. (2012) Simulation of Pavement Surface Runoff using the Depth-Averaged ShallowWater Equations. 93(März), 149.
  19. Lei et al. (2020) Study on Runoff and Infiltration for Expansive Soil Slopes in Simulated RainfallWater 12 (1) 222.
  20. Inn et al. (2020) Features of the Flow Velocity and Pressure Gradient of an Undular Bore on aHorizontal Bed Physics of fluids 32 (4) 043603.
Scouring

FLOW-3D Modelling of the Debris Effect on Maximum Scour Hole Depth at Bridge Piers

교각 주변 최대 세굴 깊이에 대한 부유물(Debris)의 영향 분석: FLOW-3D 시뮬레이션

연구 배경 및 목적

  • 문제 정의: 교각(Bridge Pier) 주변의 국부 세굴(Local Scour)은 하천 바닥의 침식을 유발하여 교량의 구조적 안전성을 위협하는 주요 요인 중 하나이다.
    • 홍수 시에는 유량 증가부유물 증가로 인해 세굴 현상이 더욱 심화된다.
    • 부유물은 교각 주변에 쌓여 흐름을 방해하고, 난류(Turbulence) 증가전단응력(Shear Stress) 증대로 이어져 세굴을 악화시킨다.
  • 연구 목적:
    • FLOW-3D CFD 모델을 사용하여 부유물 형태 및 위치가 원형 교각 주변의 최대 세굴 깊이에 미치는 영향을 평가.
    • 삼각형 및 직사각형 부유물을 수면에 떠있는 경우(floating)와 하상(sand bed)에 놓인 경우로 구분하여 비교.
    • 실험 결과와의 비교 검증을 통해 모델의 신뢰성을 평가.

연구 방법

수치 모델링 및 시뮬레이션 설정

  • FLOW-3D 소프트웨어를 활용한 3차원 CFD 해석 수행.
  • RNG k-ε 난류 모델을 사용하여 난류 흐름을 모델링.
  • VOF(Volume of Fluid) 기법을 통해 자유 수면(free surface)을 추적.
  • 모델 검증:
    • Robalo (2014)의 실험 데이터를 사용하여 평균 속도 및 세굴 깊이 비교.
    • 실험 채널은 길이 12.0m, 폭 0.83m, 높이 1.0m의 직사각형 콘크리트 플룸(fluvial hydraulic channel) 사용.
  1. 부유물(Debris) 유형 및 조건
    • 부유물 형태: 삼각형(Triangular)직사각형(Rectangular).
    • 부유물 위치:
      • 수면(floating debris): 부유물이 흐름을 막아 세굴을 증대시킴.
      • 하상(sand bed debris): 세굴 억제(countermeasure) 역할을 하여 세굴 깊이를 줄이는 효과.
    • 하상 재료:
      • 천연 석영 모래(Quartz Sand) 사용, D50 = 0.86 mm, 밀도 2666 kg/m³.
      • 평균 접근 유속(U) = 0.317 m/s, 수심 0.15 m 설정.
  2. 모델 검증 및 비교 분석
    • FLOW-3D 결과와 실험 결과 비교:
      • 평균 속도 프로파일 비교 시, 실험과 유사한 흐름 발달을 보여 모델의 신뢰성 확보.
      • 그러나 이동 가능한 하상(movable bed)을 적용했을 때, 평균 30%의 편차가 발생.
    • Shields (1936) 기준과의 비교:
      • 실험에서는 Neil (1967) 및 Garde (1970) 공식을 사용하여 한계 유속(Uc) 0.314 m/s를 평가.
      • FLOW-3D에서는 Shields 기준(Uc 0.403 m/s)을 사용하여 20% 높은 값을 적용.
      • 이는 세굴 깊이 과소 예측의 주요 원인으로 분석.

주요 결과

  1. 세굴 깊이 및 부유물 영향 비교
    • 부유물 없는 경우:
      • 세굴 깊이 0.06 m.
    • 부유물 유형에 따른 세굴 깊이:
      • 직사각형 부유물(수면): 세굴 깊이 0.07 m (가장 큰 세굴).
      • 삼각형 부유물(수면): 세굴 깊이 0.05 m.
      • 삼각형 부유물(하상): 세굴 깊이 0.04 m, 세굴 감소 효과 ≈ 40%.
  2. FLOW-3D 모델의 신뢰성 평가
    • 고정된 하상(fixed bed) 시뮬레이션에서는 실험과 높은 일치도를 보임.
    • 그러나 이동 가능한 하상(movable bed) 적용 시, 실험 결과와 평균 30% 편차 발생.
    • Shields 기준의 한계:
      • Uc 평가 방법의 차이가 주요 원인으로 분석.
      • Shields 기준은 한계 전단응력(Threshold Shear Stress)을 과대 평가하여 세굴 깊이를 과소 예측.

결론 및 향후 연구

  • 결론:
    • FLOW-3D 모델은 부유물 유형 및 위치에 따른 세굴 깊이 변화를 예측할 수 있음.
    • 수면에 떠 있는 직사각형 부유물세굴을 가장 크게 증가시키며, 삼각형 부유물(하상)은 세굴을 줄이는 효과가 있음.
    • Shields 기준의 적용세굴 깊이 과소 예측의 원인으로, 국내 하천 조건에 맞는 보정 필요.
  • 향후 연구 방향:
    • 다양한 난류 모델(예: LES, k-ω 모델) 적용 및 비교.
    • 다양한 하상 조건 및 교각 형상에 대해 추가 검증.
    • AI 및 머신러닝을 활용한 세굴 예측 모델 개발.
    • 부유물의 재질, 크기 및 배열에 따른 세굴 영향 연구.

연구의 의의

이 연구는 FLOW-3D를 활용한 교각 주변 부유물의 세굴 영향 분석을 통해 교량 설계 및 유지보수 전략 수립에 중요한 기초 데이터를 제공하며, 홍수 시 구조물 안전성을 높이는 데 기여할 수 있다​.

Reference

  1. Baykal, C., Sumer, B.M., Fuhrman, D.R., Jacobsen, N.G. e FredsØe, J. (2015). “Numerical investigation of flow and scour around a vertical circular cylinder”. Philos Trans A MAth Phys Eng Sci, 373(2033): 20140115.
  2. Dias, A.J.P. (2018). Study the impact of debris on cavities erosion at bridge piers”. MSc Thesis, University of Beira Interior (in Portuguese).
  3. Dias, A.J.P., Fael, C.S. and Núñez-González, F. (2019). Effect of debris on local scour at bridge piers. IOP Conference Series: Materials Science and Engineering, 471–022024.
  4. Franzetti, S., Radice, A., Rabitti, M. and Rossi, G. (2011). Hydraulic design and preliminary performance evaluation of countermeasure against debris accumulation and resulting local pier scour on River Po in Italy. Journal of Hydraulic Engineering, 137(5), 615–620.
  5. Garde, R.J. (1970). Initiation of motion on a hydrodynamically rough surface. Critical velocity approach, JIP 6(2) India.
  6. Ghasemi, M. and Soltani-Gerdefaramarzi, S. (2017). The Scour Bridge Simulation around a Cylindrical Pier Using Flow-3D. Journal of Hydrosciences and Environment, 1(2), 46–54.
  7. Hemdan, N.T., Abdallah, M.Y., Mohamed, A.G., Basiouny, M., Abd-Elmaged, A.B.A. (2016). Experimental study on the effect of permeable blockage at front of one pier on scour depth at mult-vents bridge supports. Journal of Engineering Sciences, Assiut University, Faculty of Engineering, 44(1), 27–39.
  8. Li, G., Lang, L. and Ning, J. (2013). 3D Numerical Simulation of Flow and Local Scour around a Spur Dike. Proceedings of the 35th IAHR World Congress, Chengdu, China.
  9. Mehnifard, M.A., Dalfardi, S., Baghdadi, H. and Seirfar, Z. (2014). Simulation of local scour caused by submerged horizontal jets with Flow-3D numerical model. Desert 20–1, 47–55.
  10. Meyer-Peter, E. and Müller, R., (1948), Formulas for bed-load transport. Proceedings of the 2nd Meeting of the International Association for Hydraulic Structures Research. 39–64.
  11. Mohamed, H.I. (2012). Numerical Simulation of Flow and Local Scour at Two Submerged-emergent Tandem Cylindrical Piers”. Journal of Engineering Sciences, Assiut University, 41(1).
  12. Moussa, Y.A.M., Nasr-Allah, T.H. and Abd-Elhasseb, A. (2016). Studying the effect of partial blockage on multivents bridge pier scour experimentally and numerically. Ain Shams Engineering Journal, 9(4), 1439-1450.
  13. Neil, C.R. (1967). Mean velocity criterion for scour of coarse uniform bed-material. Proceeding of of the XII IAHR Congress, Fort Collins, Colorado, 4654.
  14. Pagliara, S. and Carnacina, I. (2010). Temporal scour evolution at bridge piers: roughness and porosity. Journal of Hydraulic Research, 48 (1), 3–13.
  15. Rahimi, E., Qaderi, K., Rahimpour, M. and Ahmadi, M.M. (2017). Effect of Debris on Pier Group Scour: An Experimental Study. JKSCE ournal of Civil Engineering,1–10.
  16. Ramos, C. M. (2005) – Drainage in Transport Infrastructure and Bridges Hydraulics. National Laboratory for Civil Engineering, Book, Chapter C2 (in Portuguese)
  17. Robalo, R.M.T. (2014). Influence of vertical cylindrical elements permeability on flow behavior, MSc Thesis. University of Beira Interior (in Portuguese).
  18. Shields, A.F. (1936). Application of similarity principles and turbulence research to bed-load movement. Vol 26. Simarro, G., Fael, C. and Cardoso, A. (2011). Estimating equilibrium scour depth at cylindrical piers in experimental studies. Journal of Hydraulic Engineering, 137 (9), 1089–1093.
  19. Simons, D.B., and Sentürk, F. (1992). Sediment transport technology. Fort Collins, Colorado, USA, Water Resources Publications.
  20. Soulsby, R.L. and Whitehouse, R.J.S.W., (1997). Threshold of sediment motion in Coastal Environments. Proceedings of Combined Australian Coastal Engineering and Port Conference, EA, 49–154.
  21. Vasquez, J.A. and Walsh, B.W. (2009). CFD simulation of local scour in complex piers under tidal flow. Proceedings of the 33rd IAHR Congress: Water Engineering for a Sustainable Environment, Vancouver, Canada.
  22. Winterwerp, J.C., Bakker, W.T., Mastbergen, D.R. and Van Rossum, H., (1992) Hyperconcentrated sand-water mixture flows over erodible bed. Journal of Hydraulic Engineering, 118, 1508–1525.
  23. Zevenbergen, L.W., Lagasse, P.F. and Clopper, P.E. (2007). Effects of Debris on Bridge Pier Scour. World Environmental and Water Resources Congress 2007: Restoring Our Natural Habitat, 1–10
scouring

Three-Dimensional Numerical Simulation of Local Scour Around Circular Bridge Pier Using FLOW-3D Software

FLOW-3D 소프트웨어를 이용한 원형 교각 주변 국부 세굴의 3차원 수치 시뮬레이션


연구 배경 및 목적

  • 문제 정의: 교각(Bridge Pier) 주변의 국부 세굴(Local Scour)은 하천 바닥의 침식으로 인해 구조물의 안전성을 위협하는 주요 요인 중 하나이다.
  • 연구 목적: FLOW-3D를 활용하여 교각 주변의 국부 세굴 형상을 3D 시뮬레이션하고, 실험 데이터를 비교하여 모델의 신뢰성을 검증하는 것이다.
  • 핵심 기여:
    • FLOW-3D를 활용한 CFD 모델 개발: 유체 흐름과 퇴적물 이동을 고려한 세굴 시뮬레이션.
    • 실험 결과와 비교 검증: Melville 실험 데이터를 바탕으로 모델 검증 및 정확도 평가.
    • 세굴 깊이 예측 및 설계 최적화: 교각 설계 및 유지관리 전략에 적용 가능.

연구 방법

  1. 수치 모델링 및 난류 모델 적용
    • Navier-Stokes 방정식 기반 CFD 해석 수행.
    • VOF(Volume of Fluid) 기법을 활용하여 자유 수면 추적.
    • RNG k-ε 난류 모델을 사용하여 교각 주변 난류 구조를 해석.
  2. 세굴 모델링
    • Meyer-Peter & Müller 공식을 사용하여 침식 및 퇴적 거동 해석.
    • Shields Parameter를 적용하여 세굴 발생 임계값 예측.
    • Melville 실험 모델과 동일한 유속(0.25 m/s) 및 입자 크기(0.385 mm) 설정.
  3. 메쉬 설정 및 경계 조건
    • 격자 독립성 검토: 1~30 mm의 다양한 격자 크기를 적용하여 최적의 메쉬 크기(5 mm) 선정.
    • 경계 조건:
      • 입구: 일정한 유속(0.25 m/s) 설정.
      • 출구: 자유 유출 조건 적용.
      • 하천 바닥: 이동 가능 침전층(Sediment Bed)으로 설정.

주요 결과

  1. 세굴 깊이 비교
    • 실험 값: 4.00 cm
    • Flow-3D 예측값: 3.6 cm (실험 대비 오차 10%)
    • 시뮬레이션 결과와 실험 데이터 간 높은 상관관계 확인.
  2. 유동장 및 세굴 형상 분석
    • 세굴 패턴: 교각 전면부에서 강한 와류(Horseshoe Vortex) 발생 → 침식 심화.
    • 교각 후류(Downstream) 영역: 유속이 급격히 감소하며 침전 형성.
    • RNG k-ε 모델 적용 효과: 세굴 깊이 및 와류 구조를 효과적으로 예측.
  3. 메쉬 크기의 영향
    • 5mm 이하의 세밀한 격자에서 최적의 결과 도출.
    • 30mm 이상의 거친 격자에서는 세굴 깊이가 과소 예측됨.

결론 및 향후 연구

  • FLOW-3D 기반 세굴 시뮬레이션이 실험 결과와 높은 정확도로 일치함을 확인.
  • RNG k-ε 난류 모델이 교각 주변의 난류 구조 및 세굴 깊이 예측에 적합함을 입증.
  • 향후 연구에서는 LES(Large Eddy Simulation) 모델과 비교, 다양한 교각 형상 및 유량 조건에서 추가 검증이 필요.

연구의 의의

이 연구는 FLOW-3D를 활용하여 교각 주변 국부 세굴을 정량적으로 분석하는 방법론을 제시하며, 교량 설계 및 유지보수 전략 수립에 활용될 수 있는 중요한 기초 데이터를 제공한다​.

Reference

  1. Breusers Nicollet and Shen 1977 Local scour around cylindrical piers Journal of Hydraulic Research, IAHR,15 (3): 211-252.
  2. Shepherd R. and Frost J D 1995 Failures in civil engineering: Structural, foundation and geoenvironmental case studies Journal of Hydraulic Engineering, Puolisher ASCE.
  3. Cheremisinoff N P and Cheng S L 1987 Hydraulic mechanics 2 Civil Engineering Practice, Technomic Published Company, Lancaster, Pennsylvania, U.S.A. 780 p.
  4. Melville B W 1975 Local scour at bridge sites University of Auckland, New Zealand, phd. Thesis, Dept. of Civil eng., Rep. No. 117.
  5. Abdul-Nour M 1990 Scouring depth around multiple M.Sc. Thesis , Department of Irrigation and Drainage , University of Baghdad.
  6. Hosny M M 1995 Experimental study of local scour around circular bridge piers in cohesive soils Colorado State University, Fort Collins.
  7. Ansari S A Kothyari U C and Ranga Raju K G 2002 Influence of cohesion on scour around bridge piers Journal of Hydraulic Research, IAHR, pp. 40(6): 717-729.
  8. Khsaf S I 2010 A study of scour around Al-Kufa bridge piers Kufa Engineering Journal.Vol.1No.1,2010, University of Kufa / College Engineering / Civil Department.
  9. Hassan W H Jassem M H and Mohammed S S 2018 A GA-HP Model for the Optimal Design of Sewer Networks Water Resour. Manag., vol. 32, no. 3, pp. 865–879.
  10. Hassan W H 2017 Application of a genetic algorithm for the optimization of a cutoff wall under hydraulic structures J. Appl. Water Eng. Res., vol. 5, no. 1, pp. 22–30, Jan.
  11. Ataie-Ashtiani B 2013 Flow field around single and tandem piers Flow Turbulence and Combustion Journal of Hydraulic Engineering,volume 9429.
  12. Flow -3D manual 2014 Flow-3D user manual version 11, Flow Science Santa Fe, NM.
  13. Richardson J E and Panchang V G 1998 Three-Dimensional Simulation of Scour Inducing Flow at Bridge Piers Journal of Hydraulic Engineering, 124(5), pp. 530–540. doi: 10.1061/(asce)0733- 9429(1998)124:5(530).
  14. Vasquez J and Walsh B 2009 CFD simulation of local scour in complex piers under tidal flow Proceedings of the thirty-third IAHR Congress: Water Engineering for a Sustainable Environment, (604), pp. 913–920.
  15. W H H and Halah k Jalal 2019 Effect of Bridge Pier Shape on Depth of Scour Iop, Conf. Ser.,(under puplication).
  16. Obeid Z H 2016 3D numerical simulation of local scouring and velocity distributions around bridge piers with different shapes A Peer Reviewed International Journal of Asian Academic Research Associates, 20(16), p. 2801. doi: 10.1186/1757-7241-20-67.
  17. Drikakis D 2003 Advances in turbulent flow computations using high-resolution methods Progress in Aerospace Sciences, 39(6–7), pp. 405–424. doi: 10.1016/S03760421(03)00075-7.
  18. Yakhot and Orszag 1986 Renormalization Group Analysis of Turbulence, Basic Theory Journal of Scientific Computing, pp. 3–51. 1, pp. 3–51.
  19. Mastbergen D R and Van Den Berg J H 2003 Breaching in fine sands and the generation of sustained turbidity currents in submarine canyons Sedimentology, 50(4), pp. 625–637. doi: 10.1046/j.1365-3091.2003.00554.x.
  20. Soulsby R L and Whitehouse R J S W 1997 Threshold of sediment motion in Coastal Environments Proc. Combined Australian Coastal Engineering and Port Conference, EA, pp. 149-154.
  21. Meyer-Peter E and Müller R 1948 Formulas for bed-load transport Proceedings of the 2nd Meeting of the International Association for Hydraulic Structures Research, 39– 64.
  22. Wei G Brethour J Grünzner M and Burnham J 2014 Sedimentation Scour Model Flow Science Report 03-14.
Fluid Velocity

Modeling of Local Scour Depth Around Bridge Pier Using FLOW-3D

FLOW-3D를 이용한 교각 주변 국부 세굴 깊이 모델링


연구 배경 및 목적

  • 문제 정의: 교각 주변에서 발생하는 국부 세굴(Local Scour)은 하천 바닥 침식을 유발하여 교량의 구조적 안정성을 위협하는 주요 요인 중 하나이다.
  • 연구 목적:
    • FLOW-3D를 활용한 세굴 모델 개발: CFD(Computational Fluid Dynamics) 기반 수치 모델을 사용하여 교각 주변의 세굴 형상을 예측.
    • 실험 데이터와의 비교: 실험실 실험과 수치 모델의 결과를 비교하여 모델의 신뢰성을 평가.
    • 세굴 깊이 및 유속 패턴 분석: 교각 앞쪽 및 후류에서 형성되는 유동 구조와 세굴의 관계를 분석.

연구 방법

  1. 실험 데이터 수집 및 모델링
    • 실험실 실험:
      • 터키 가지안테프 대학교의 수리 실험실에서 수행.
      • 0.8m × 0.9m 크기의 직사각형 수로에서 직경 10cm의 원형 교각을 배치.
      • 유량 0.048 m³/s, 유속 0.48 m/s, 수심 11cm 설정.
      • 세굴층은 비응집성(non-cohesive) 모래(d₅₀ = 1.45mm)로 구성.
    • FLOW-3D 기반 CFD 모델링:
      • VOF(Volume of Fluid) 기법을 사용하여 자유 수면 모델링.
      • RNG k-ε 난류 모델을 적용하여 난류 흐름 분석.
      • 침식 및 퇴적 모델을 적용하여 하상 변화 예측.
  2. 격자 설정 및 경계 조건
    • 메쉬 독립성 검토: 64,000개 이상의 격자를 사용하여 최적화 수행.
    • 경계 조건:
      • 입구: 일정한 유속(0.48 m/s) 설정.
      • 출구: 자유 유출 조건 적용.
      • 하천 바닥: 이동 가능 침전층(Sediment Bed)으로 설정.

주요 결과

  1. 세굴 깊이 비교
    • 실험 값: 6.9 cm
    • FLOW-3D 예측값: 6.5 cm (실험 대비 오차 10%)
    • 실험과 수치 모델의 결과가 높은 상관관계를 보임.
  2. 유동 및 세굴 패턴 분석
    • 유속 분포:
      • 교각 전면부에서 강한 와류(Horseshoe Vortex) 발생 → 침식 심화.
      • 후류 영역에서는 유속이 감소하며 퇴적 형성.
    • 세굴 형상:
      • 최대 세굴 깊이는 교각 전면부 및 측면에서 발생.
      • FLOW-3D 모델은 세굴 발생 위치 및 심도를 효과적으로 예측.
  3. 시간에 따른 세굴 발전
    • 실험 및 CFD 모델 모두에서 1시간 후 세굴 깊이가 안정화됨.
    • 세굴 속도는 초기 30분 동안 급격히 증가한 후 점진적으로 감소.

결론 및 향후 연구

  • 결론:
    • FLOW-3D 기반 CFD 모델은 교각 주변의 세굴 깊이를 실험 결과와 높은 정확도로 예측할 수 있음.
    • RNG k-ε 난류 모델이 국부 세굴 해석에 적합함을 확인.
    • 세굴 깊이 예측에서 실험 대비 오차는 약 10%로 양호한 결과를 보임.
  • 향후 연구 방향:
    • 더 정교한 난류 모델(예: LES) 적용 및 비교.
    • 다양한 교각 형상 및 유량 조건에서 추가 검증.
    • 인공지능(AI) 및 머신러닝을 활용한 세굴 예측 모델 개발.

연구의 의의

이 연구는 FLOW-3D를 이용한 국부 세굴 예측의 신뢰성을 검증하고, 교량 설계 및 유지보수 전략 수립에 활용될 수 있는 중요한 기초 데이터를 제공한다.

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Scouring

3D Numerical Simulation of Flow Field Around Twin Piles

쌍둥이 말뚝 주변 유동장에 대한 3차원 수치 시뮬레이션


연구 배경 및 목적

  • 문제 정의: 교각이나 말뚝(pile) 주위에서 발생하는 국부적인 세굴(scour)은 구조물의 안정성에 중요한 영향을 미친다.
  • 연구 목적: FLOW-3D 소프트웨어를 이용하여 두 개의 말뚝(쌍둥이 말뚝) 주위의 유동 패턴과 세굴 메커니즘을 수치적으로 시뮬레이션하고, 실험 데이터를 활용하여 검증하는 것이다.

연구 방법

  1. 수치 모델링 및 난류 모델
    • FLOW-3D 소프트웨어를 사용하여 RNG k-ε 난류 모델을 기반으로 유동 해석 수행.
    • 말뚝의 배치: 병렬(side-by-side) 배치직렬(tandem) 배치 두 가지를 고려.
    • 실험 데이터와 비교하여 모델의 신뢰성을 검증.
  2. 계산 영역 및 격자(Grid) 설정
    • 비균일(non-uniform) 격자 분포를 사용하여 말뚝 주변의 유동을 정밀하게 모델링.
    • 최소 격자 크기: 0.009 m, 최대 격자 크기: 0.039 m.
    • 메쉬 개수: x 방향 400개, y 방향 110개, z 방향 40개.
  3. 경계 조건
    • 유입 속도 및 압력을 각각 입출력 경계 조건으로 설정.
    • 상류에서 개발된 유동을 프로파일로 생성하여 말뚝이 존재하는 구역의 유입 경계 조건으로 적용.

주요 결과

  1. 유동 패턴 분석
    • 병렬 배치(Side-by-side):
      • 말뚝 사이에서 제트(Jet) 유동이 발생하며 비대칭적인 흐름 형성.
      • 배치 간격이 증가할수록 후류(Vortex shedding) 현상이 뚜렷해짐.
    • 직렬 배치(Tandem):
      • 앞쪽 말뚝이 후방 말뚝을 보호하는 Sheltering 효과 발생.
      • Reynolds 수와 배치 간격(S/d)에 따라 와류 형성 패턴이 변화.
      • 후류에서 강한 난류 구조가 나타나며, Wake Vortex가 형성됨.
  2. 실험과의 비교
    • 실험 데이터와 시뮬레이션 결과를 비교한 결과, 전반적으로 유동 패턴이 잘 일치함.
    • 그러나 말뚝 사이의 복잡한 유동장에서는 일부 차이가 발생하여 추가적인 모델 보정이 필요함.
  3. Reynolds 수와 배치 간격의 영향
    • 말뚝 간 간격(S/d)이 증가할수록 앞쪽 말뚝의 보호 효과가 감소하고, 후방 말뚝 주변에서 강한 와류가 형성됨.
    • 낮은 Reynolds 수에서는 단일 말뚝과 유사한 흐름 패턴을 보이나, 높은 Reynolds 수에서는 와류가 더욱 강하게 나타남.

결론 및 향후 연구

  • FLOW-3D를 활용한 3D 유동 시뮬레이션은 말뚝 주변 유동 패턴과 세굴 메커니즘을 효과적으로 분석할 수 있음을 확인함.
  • 실험 데이터와 전반적으로 높은 일치도를 보였으나, 말뚝 사이의 복잡한 유동장에서 추가적인 모델 개선이 필요함.
  • 향후 연구에서는 더 다양한 Reynolds 수와 배치 조건을 고려한 추가 실험 및 난류 모델 비교 분석이 필요함.

연구의 의의

이 연구는 교량 기초 및 해양 구조물 설계에서 말뚝 주변의 유동과 세굴 예측을 정밀하게 분석할 수 있는 CFD 기반 접근법을 제시하였으며, 향후 말뚝 배치 최적화 및 구조물 안전성 향상에 기여할 수 있음을 시사한다.

Reference

  1. Akilli AA, Karakus C (2004) Flow characteristics of circular cylinders arranged side-by- side in shallow water. Flow Meas Instrum 15(4):187–189
  2. Amini A, Mohammad TM (2017) Local scour prediction in complex pier. Mar Georesour Geotechnol 35(6):857–864
  3. Amini A, Melville B, Thamer M, Halim G (2012) Clearwater local scour around pile groups in shallow-water flow. J Hydraul Eng (ASCE) 138(2):177–185
  4. Amini A, Mohd TA, Ghazali H, Bujang H, Azlan A (2011) A local scour prediction method for pile cap in complex piers. ICE-water Manag. 164(2):73–80
  5. Aslani A (2008) Experimental evaluation of flow pattern around double piles. MSc thesis, Sharif University, Tehran Gu ZF, Sun TF (1999) On interference between two circular cylinders in staged arrangement at high sub-critical Reynolds numbers. J Wind Eng Ind Aerodyn 80:287–309
  6. Hang-Wook P, Hyun P, Yang-Ki C (2014) Evaluation of the applicability of pier local scour formulae using laboratory and field data. Mar Georesour Geotechnol. https://doi.org/10.1080/1064119X.2014.954658
  7. Hannah CR (1978) Scour at pile groups. Research Rep. No. 78-3, Civil Engineering, Univ. of Canterbury, Christchurch Hosseini R, Amini A (2015) Scour depth estimation methods around pile groups. J Civ Eng KSCE 19(7):2144–2156
  8. Lanca R, Fael C, Maia R, Peˆgo J, Cardoso A (2013) Clear-water scour at pile groups. J Hydraul Eng. https://doi.org/10.1061/(ASCE)HY.1943-7900.0000770
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pile

FLOW-3D 모형을 이용한 해상풍력기초 세굴현상 분석

연구 배경

  • 해상풍력 발전 기초는 파랑 조건에 의해 주변 유동이 크게 교란되어 세굴(Scour) 현상이 발생할 수 있다.
  • 기초의 안정성 확보를 위해 세굴 현상을 정확하게 예측하는 것이 필수적이다.
  • 본 연구는 Flow-3D를 활용하여 해상풍력기초(모노파일 및 삼각대 파일) 주변의 세굴현상을 수치해석하였다.

연구 방법

  1. 모형 설정 및 입력 조건
    • 해상풍력기초 형상: 직경이 다른 모노파일(예: D = 5.0 m, d = 1.69 m)과 동일한 직경의 모노파일, 그리고 삼각대 파일 형식을 대상으로 분석.
    • 경계조건: 상류경계에 관측 유속(약 1.066 m/s) 및 극치파랑 조건을 적용하여 세굴현상을 평가.
    • 난류 모형: LES 모형과 RNG 모형을 각각 적용하여 세굴 깊이 및 분포에 미치는 영향을 비교.
  2. 수치 해석 기법
    • Flow-3D 모형을 이용하여 3차원 유동해석을 수행.
    • FAVOR 기법과 VOF(Volume of Fluid) 방법을 사용해 복잡한 경계와 자유 표면을 정확히 재현.
    • 메쉬 독립성 및 민감도 분석을 통해 계산의 신뢰성을 확보함.

주요 결과

  • 모노파일 분석:
    • 서로 다른 직경의 모노파일에서는 최대 세굴심이 약 4.13 m로 나타났으며, 동일한 직경의 모노파일에서는 하강류가 증가하여 최대 세굴심이 약 7.13 m로 증가함.
    • 이는 동일 직경 모노파일에서 유속이 더욱 빨라지며, 세굴 현상이 심화됨을 시사함.
  • 삼각대 파일 분석:
    • 상류 경계조건으로 관측 유속과 극치파랑 조건을 각각 적용한 결과, 극치파랑 조건에서는 최대 세굴심이 약 1.3배 정도 더 깊게 발생함.
  • 난류 모형 비교:
    • LES 모형을 적용한 경우, 세굴심이 일정 시간이 경과하면 평형상태에 도달함.
    • 반면, RNG 모형은 전체 해석 영역에서 계속해서 세굴현상이 발생하여 평형상태에 도달하지 않음.
    • 따라서 해상풍력기초 세굴 해석에는 LES 모형과 극치파랑 조건의 적용이 타당함.

결론 및 향후 연구

  • 해상풍력기초에 대한 세굴현상 분석에서는 동일 직경 모노파일보다 서로 다른 직경의 파일 형식이 기초 안정성 측면에서 유리할 수 있음.
  • LES 난류 모형과 극치파랑 조건을 적용하는 것이 실제 세굴현상을 더 정확하게 예측할 수 있음을 확인함.
  • 향후 연구에서는 다양한 해양 파랑 조건 및 추가 난류 모형 비교를 통해 보다 정밀한 세굴예측 모델을 개발할 필요가 있음.

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  6. KEPRI. 『Test Bed for 2.5GW Offshore Wind Farm atYellow Sea』 Interim Design Report(in Korea), 2014.
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  10. V. Yakhot, S. A. Orszag, S. Thangam, T. B. Gatski, C.G. Speziale, “Development of turbulence models forshear flows by a double expansion technique”, Physicsof Fluids, vol. 4, no. 7, pp. 1510-1520, 1992.DOI: https://doi.org/10.1063/1.858424
FLOW

Numerical Modelling of Flow Characteristics Over Sharp Crested Triangular Hump

날카로운 정상부를 가진 삼각형 허들(Sharp-Crested Triangular Hump) 위의 유동 특성 수치 모델링


연구 배경

  • 문제 정의: 수리 구조물의 성능 및 수면 프로파일을 정확히 예측하는 것은 실험적으로 어렵고 비용이 많이 듦.
  • 목표: CFD(Computational Fluid Dynamics)를 활용하여 삼각형 허들 위의 유동 특성을 보다 효율적이고 정확하게 분석.
  • 접근법: FLOW-3D 기반 시뮬레이션을 수행하여 실험 데이터와 비교 검증.

연구 방법

  1. 삼각형 허들(Weir) 개요
    • 위어(Weir)는 개수로에서 유량 조절과 방류 역할을 수행하는 중요한 수리 구조물.
    • 본 연구에서는 크기가 50 cm × 30 cm × 7 cmSharp-Crested Triangular Hump 모델을 사용.
  2. 수치 모델링
    • FLOW-3D를 사용하여 RANS(Reynolds-Averaged Navier-Stokes) 방정식과 VOF(Volume of Fluid) 방법을 적용.
    • FAVOR(Fractional Area-Volume Obstacle Representation) 기법을 사용하여 메쉬 내 장애물 영향을 반영.
    • 1,920,000개의 격자 셀을 사용하여 시뮬레이션 수행.
  3. 실험 설정
    • Universiti Teknologi PETRONAS(UTP)의 수리 실험실에서 실험 수행.
    • 30cm 폭, 60cm 높이, 10m 길이의 플룸(flume)에서 실험 진행.
    • 4가지 유량 조건(30, 51.3, 75.3, 31 m³/h) 및 경사 조건(0, 0.006, 0.01)으로 실험 설계.

주요 결과

  1. 수치 시뮬레이션 vs 실험 데이터 비교
    • 수치 시뮬레이션과 실험 결과 간의 차이는 4~5% 이내로 매우 높은 정확도를 보임.
    • 수면 프로파일, 평균 유속, 프로우드 수(Froude Number) 등이 실험과 잘 일치.
  2. 유동 특성 분석
    • 프라우드 수(Froude Number) 변화:
      • 상류(Upstream)에서는 Froude Number < 1.0 → 서브크리티컬(Subcritical) 흐름.
      • 하류(Downstream)에서는 Froude Number > 1.0 → 슈퍼크리티컬(Supercritical) 흐름.
    • 유속(Flow Velocity) 변화:
      • 하류로 갈수록 유속 증가, 삼각형 허들이 흐름을 방해하면서 압력 변화를 유발.
    • 수심(Flow Depth) 변화:
      • 상류에서는 높은 수심 유지, 하류에서는 급격한 감소 확인.
  3. 수치 시뮬레이션의 유용성
    • FLOW-3D가 삼각형 허들 및 수리 구조물의 유동 해석에 효과적임을 확인.
    • 기존의 실험적 접근보다 비용이 낮고 신속한 설계 검토 가능.

결론 및 향후 연구

  • FLOW-3D 기반 CFD 시뮬레이션이 삼각형 허들의 유동 해석 및 설계 최적화에 효과적임을 검증.
  • 실험 데이터와 비교했을 때 높은 정확도(오차 4~5%)를 나타내며, 초기 설계 검토에 유용함.
  • 향후 연구에서는 다양한 난류 모델(k-ε, RNG, LES) 적용 및 추가적인 수리 구조물 연구가 필요.

연구의 의의

이 연구는 수리 구조물의 유동 해석을 위해 CFD 시뮬레이션을 실험적으로 검증하여, 위어 및 삼각형 허들 설계의 최적화 및 성능 예측을 위한 신뢰성 높은 방법론을 제시했다는 점에서 큰 의미가 있다.

Reference

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Weir

Discharge Formula and Hydraulics of Rectangular Side Weirs in the Small Channel and Field Inlet

소규모 수로 및 유입구에서의 직사각형 측면 위어의 유량 공식 및 수리학

Yingying Wang, Mouchao Lv, Wen’e Wang, Ming Meng

Abstract


In this study, experimental investigations were conducted on rectangular side weirs with different widths and heights. Corresponding simulations were also performed to analyze hydraulic characteristics including the water surface profile, flow velocity, and pressure. The relationship between the discharge coefficient and the Froude number, as well as the ratios of the side weir height and width to upstream water depth, was determined. A discharge formula was derived based on a dimensional analysis. The results demonstrated good agreement between simulated and experimental data, indicating the reliability of numerical simulations using FLOW-3D software (version 11.1). Notably, significant fluctuations in water surface profiles near the side weir were observed compared to those along the center line or away from the side weir in the main channel, suggesting that the entrance effect of the side weir did not propagate towards the center line of the main channel. The proposed discharge formula exhibited relative errors within 10%, thereby satisfying the flow measurement requirements for small channels and field inlets.

1. Introduction


Sharp crested weirs are used to obtain discharge in open channels by solely measuring the water head upstream of the water. Side weirs, as a kind of sharp-crested weir, are extensively used for flow measurement, flow diversion, and flow regulation in open channels. Side weirs can be placed directly in the channel direction or field inlet, without changing the original structure of the channel. Thus, side weirs have certain advantages in the promotion and application of flow measurement facilities in small channels and field inlets. The rectangular sharp-crested weir is the most commonly available, and many scholars have conducted research on it.
Research on side weirs started in 1934. De Marchi studied the side weir in the rectangular channel and derived the theoretical formula based on the assumption that the specific energy of the main flow section of the rectangular channel in the side weir section was constant [1]. Ackers discussed the existing formulas for the prediction of the side weir discharge coefficient [2]. Chen concluded that the momentum theorem was more suitable for the analytical calculation of the side weir based on the experimental data [3]. Based on previous theoretical research, more and more scholars began to carry out experimental research on side weirs. Uyumaz and Muslu conducted experiments under subcritical and supercritical flow regimes and derived expressions for the side weir discharge and water surface profiles for these regimes by comparing them with experimental results [4]. Borghei et al. developed a discharge coefficient equation for rectangular side weirs in subcritical flow [5]. Ghodsian [6] and Durga and Pillai [7] developed a discharge coefficient equation of rectangular side weirs in supercritical flow. Mohamed proposed a new approach based on the video monitoring concept to measure the free surface of flow over rectangular side weirs [8]. Durga conducted experiments on rectangular side weirs of different lengths and sill heights and discussed the application of momentum and energy principles to the analysis of spatially varied flow under supercritical conditions. The results showed that the momentum principle was fitting better [7]. Omer et al. obtained sharp-crested rectangular side weirs discharge coefficients in the straight channel by using an artificial neural network model for a total of 843 experiments [9]. Emiroglu et al. studied water surface profile and surface velocity streamlines, and developed a discharge coefficient formula of the upstream Froude number, the ratios of weir length to channel width, weir length to flow depth, and weir height to flow depth [10]. Other investigators [11,12,13,14] have conducted experiments to study flow over rectangular side weirs in different flow conditions.
Numerous studies have been conducted in laboratories to this day. Compared to experimental methods, the numerical simulation method has many attractive advantages. We can easily obtain a wide range of hydraulic parameters of side weirs using numerical simulation methods, without investing a lot of manpower and resources. In addition, we can conduct small changes in inlet condition, outlet condition, and geometric parameters, and study their impact on the flow characteristics of side weirs. Therefore, with the development and improvement of computational fluid dynamics, the numerical simulation method has begun to be widely applied on side weirs. Salimi et al. studied the free surface changes and the velocity field along a side weir located on a circular channel in the supercritical regime by numerical simulation [15]. Samadi et al. conducted a three-dimensional simulation on rectangular sharp-crested weirs with side contraction and without side contraction and verified the accuracy of numerical simulation compared with the experimental results [16]. Aydin investigated the effect of the sill on rectangular side weir flow by using a three-dimensional computational fluid dynamics model [17]. Azimi et al. studied the discharge coefficient of rectangular side weirs on circular channels in a supercritical flow regime using numerical simulation and experiments [18]. The discharge coefficient over the two compound side weirs (Rectangular and Semi-Circle) was modeled by using the FLOW-3D software to describe the flow characteristics in subcritical flow conditions [19]. Safarzadeh and Noroozi compared the hydraulics and 3D flow features of the ordinary rectangular and trapezoidal plan view piano key weirs (PKWs) using two-phase RANS numerical simulations [20]. Tarek et al. investigated the discharge performance, flow characteristics, and energy dissipation over PK and TL weirs under free-flow conditions using the FLOW-3D software [21].
As evident from the aforementioned, the majority of studies have primarily focused on determining the discharge coefficient, while comparatively less attention has been devoted to investigating the hydraulic characteristics of rectangular side weirs. Numerical simulations were conducted on different types of side weirs, including compound side weirs and piano key weirs, in different cross-section channels under different flow regimes. It is imperative to derive the discharge formula and investigate other crucial flow parameters such as depth, velocity, and pressure near side weirs for their effective implementation in water measurement. In this study, a combination of experimental and numerical simulation methods was employed to examine the relationship between the discharge coefficient and its influencing factors; furthermore, a dimensionless analysis was utilized to derive the discharge formula. Additionally, water surface profiles near side weirs and pressure distribution at the bottom of the side channel were analyzed to assess safety operation issues associated with installing side weirs.

2. Principle of Flow Measurement


Flow discharge over side weirs is a function of different dominant physical and geometrical quantities, which is defined as

where Q is flow discharge over the side weir, b is the side weir width, B is the channel width, P is the side weir height, v is the mean velocity, h1 is water depth upstream the side weir in the main channel, g is the gravitational acceleration, μ is the dynamic viscosity of fluid, ρ is fluid density, and i is the channel slope (Figure 1).

Figure 1. Definition sketch of parameters of rectangular side weir under subcritical flow. Note: h1 and h2 represent water depth upstream and downstream of the side weir in the main channel, respectively; y1 and y2 represent weir head upstream and downstream of the side weir in the main channel, respectively.

In experiments when the upstream weir head was over 30 mm, the effects of surface tension on discharge were found to be minor [22]. The viscosity effect was far less than the gravity effect in a turbulent flow. Hence μ and σ were excluded from the analysis [23,24]. In addition, the channel width, the channel slope, and the fluid density were all constant, so the discharge formula can be simplified as:

According to the Buckingham π theorem, the following relationship among the dimensionless parameters is established:

Selected h1 and g as basic fundamental quantities, and the remaining physical quantities were represented in terms of these fundamental quantities as follows:

In which

Based on dimensional analysis, the following equations were derived.

Namely

So the discharge formula can be simplified as:

In a sharp-crested weir, discharge over the weir is proportional to 𝐻1.51H11.5 (H1 is the upstream total head above the crest, namely H1 = y1 + v2/2 g), so Equation (6) can be transformed as follows:

Consequently, the discharge formula over rectangular side weirs is defined as follows, in which 𝑚=𝑓(𝑏ℎ1m=f(bh1,𝑃ℎ1,𝐹𝑟1)Ph1,Fr1). Parameter m represents the dimensionless discharge coefficient. Parameter Fr1 represents the Froude number at the upstream end of the side weir in the main channel.

3. Experiment Setup


The experimental setup contained a storage reservoir, a pumping station, an electromagnetic flow meter, a control valve, a stabilization pond, rectangular channels, a side weir, and a sluice gate. The layout of the experimental setup is shown in Figure 2. Water was supplied from the storage reservoir using a pump. The flow discharge was measured with an electromagnetic flow meter with precision of ±3‰. Water depth was measured with a point gauge with an accuracy of ±0.1 mm. The flow velocity was measured with a 3D Acoustic Doppler Velocimeter (Nortek Vectrino, manufactured by Nortek AS in Rud, Norway). In order to eliminate accidental and human error, multiple measurements of the water depth and flow velocity at the same point were performed and the average values were used as the actual water depth and flow velocity of the point. The main and side channels were both rectangular open channels measuring 47 cm in width and 60 cm in height. The geometrical parameters of rectangular side weirs are shown in Table 1.

Figure 2. Layout of the test system.
Table 1. The geometrical parameters of rectangular side weirs.

When water passes through a side weir, its quality point is affected not only by gravity but also by centrifugal inertia force, leading to an inclined water surface within that particular cross-section before reaching the weir. In order to examine water profiles adjacent to side weirs, cross-sectional measurements were conducted at regular intervals of 12 cm both upstream and downstream of each side weir, denoted as sections ① to ⑩, respectively. Measuring points were positioned near the side weir (referred to as “Side I”), along the center line of the main channel (referred to as “Side II”), and far away from the side weir (referred to as “Side III”) for each cross-section. The schematic diagram illustrating these measuring points is presented in Figure 3.

Figure 3. Schematic diagram of measurement points.

4. Numerical Simulation Settings

4.1. Mathematical Model

4.1.1. Governing Equations

Establishing the controlling equations is a prerequisite for solving any problem. For the flow analysis problem of water flowing over a side weir in a rectangular channel, assuming that no heat exchange occurs, the continuity equation (Equation (9)) and momentum equation (Equation (10)) can be used as the controlling equations as follows:

The continuity equation:

Momentum equation:

where: ρ is the fluid density, kg/m3t is time, s; uiuj are average flow velocities, u1u2u3 represent average flow velocity components in Cartesian coordinates x, y, and z, respectively, m/s; μ is dynamic viscosity of fluid, N·s/m2p is the pressure, pa; Si is the body force, S1 = 0, S2 = 0, S3 = −ρg, N [24].

4.1.2. RNG k-ε Model

The water flow in the main channel is subcritical flow. When the water flows through the side weir, the flow line deviates sharply, the cross section suddenly decreases, and due to the blocking effect of the side weir, the water reflects and diffracts, resulting in strong changes in the water surface and obvious three-dimensional characteristics of the water flow [25]. Therefore the RNG kε model is selected. The model can better handle flows with greater streamline curvature, and its corresponding k and ε equation is, respectively, as follows:

where: k is the turbulent kinetic energy, m2/s2μeff is the effective hydrodynamic viscous coefficient; Gk is the generation item of turbulent kinetic energy k due to gradient of the average flow velocity; C∗1εC1ε*, C are empirical constants of 1.42 and 1.68, respectively; ε is turbulence dissipation rate, kg·m2/s2.

4.1.3. TruVOF Model

Because the shape of the free surface is very complex and the overall position is constantly changing, the fluid flow phenomenon with a free surface is a typical flow phenomenon that is difficult to simulate. The current methods used to simulate free surfaces mainly include elevation function method, the MAC method [26] and the VOF (Volume of Fluid) method [27]. The VOF method is a method proposed by Hirt and Nichols to deal with the complex motion of the free surface of a fluid, which can describe all the complexities of the free surface with only one function. The basic idea of the method is to define functions αw and αa, which represent the volume percentage of the calculation area occupied by water and air, respectively. In each unit cell, the sum of the volume fractions of water and air is equal to 1, i.e.,

The TruVOF calculation method can accurately track the change of free liquid level and accurately simulate the flow problems with free interface. Its equation is:

where: u_¯m is the average velocity of the mixture; t is the time; F is the volume fraction of the required fluid.

4.2. Parameter Setting and Boundary Conditions

To streamline the iterative calculation and minimize simulation time, we selected a main channel measuring 7.5 m in length and a side channel measuring 2.5 m in length for simulation. Three-dimensional geometrical models were developed using the software AutoCAD (version 2016-Simplified Chinese). The spatial domain was meshed using a constructed rectangular hexahedral mesh and each cell size was 2 cm. A volume flow rate was set in the channel inlet with an auto-adjusted fluid height. An outflow–outlet condition was positioned at the end of the side channel. A symmetry boundary condition was set in the air inlet at the top of the model, which represented that no fluid flows through the boundary. The lower Z (Zmin) and both of the side boundaries were treated as a rigid wall (W). No-slip conditions were applied at the wall boundaries. Figure 4 illustrates these boundary conditions.

Figure 4. Diagram of boundary conditions.

5. Results

5.1. Water Surface Profiles

Water surface profiles were crucial parameters for selecting water-measuring devices. Upon analyzing the consistent patterns observed in different conditions, one specific condition was chosen for further analysis. To validate the reliability of numerical simulation, measured and simulated water depths of rectangular side weirs with different widths and heights at a discharge rate of 25 L/s were extracted for comparison (Table 2 and Figure 5). The results in Table 2 and Figure 5 indicate a maximum absolute relative error value of 9.97% and all absolute relative error values within 10%, demonstrating satisfactory agreement between experimental and simulated results.

Figure 5. Comparison between measured and simulated flow depth.
P/cmSection Positionb = 20 cmb = 30 cmb = 40 cmb = 47 cm
hm/cmhs/cmR/%hm/cmhs/cmR/%hm/cmhs/cmR/%hm/cmhs/cmR/%
721.4919.49.7317.7416.94.7416.0714.519.7113.7912.509.35
④′20.4819.056.9817.7816.149.2215.6914.318.80
20.7119.028.1617.8216.318.4715.9214.538.7315.2313.809.39
⑧′22.0020.228.0918.2716.748.3716.5914.969.83
22.3720.179.8317.7316.805.2516.2715.087.3115.3614.366.51
1024.1522.66.4219.9618.845.6119.0318.582.3616.8315.855.82
④′24.2122.058.9219.4918.196.6718.7518.352.13
24.0121.789.2919.6518.346.6718.9518.631.6917.5216.098.16
⑧′24.8822.49.9720.6519.216.9720.1219.294.13
24.0322.964.4521.1619.348.6019.7119.431.4218.3917.365.60
1528.8527.564.4725.8624.096.8424.0521.898.9822.7320.808.49
④′28.4926.975.3425.1923.845.3623.4221.468.37
28.8526.986.4825.7223.996.7323.2321.826.0723.1021.058.87
⑧′28.9627.305.7326.3824.198.3024.1822.277.90
29.1827.964.1826.5724.547.6424.5722.339.1223.2021.109.05
2033.2932.342.8530.6329.025.2628.4926.875.6926.9925.814.37
④′33.1431.953.5929.7528.623.8028.1126.794.70
33.3231.794.5930.0428.455.2928.9926.867.3527.4226.722.55
⑧′34.0232.394.7930.6928.955.6729.5927.257.91
34.6232.845.1431.4429.296.8429.5127.317.4628.2127.004.29
Table 2. Comparison of measured and simulated water depths on Side I of each side weir at a discharge of 25 L/s

Due to the diversion caused by the side weir, there was a rapid variation in flow near the side weir in the main channel. In order to investigate the impact of the side weir on water flow in the main channel, water surface profiles on Side I, Side II, and Side III were plotted with a side weir width and height both set at 20 cm at a discharge rate of 25 L/s (Figure 6). As depicted in Figure 6, within a certain range of the upstream end of the main channel, water depths on Side I, Side II, and Side III were nearly equal with almost horizontal profiles. As the distance between the location of water flow and the upstream end of the weir crest decreased gradually, there was a gradual decrease in water depth on Side I along with an inclined trend in its corresponding profile; however, both Side II and Side III still maintained almost horizontal profiles. When approaching closer to the side weir area with flowing water, there was an evident reduction in water depth on Side I accompanied by a significant downward trend visible across an expanded decline range. The minimum point occurred near the upstream end of the weir crest before gradually increasing again towards downstream sections. At the crest section of the side weir, there is an upward trend observed in the water surface. The water surface tended to stabilize downstream of the main channel within a certain range from the downstream end of the weir crest. There was no significant change in the water surface profiles of Side Ⅱ and Side Ⅲ in the crest section. It can be inferred that the side weir entrance effect occurred only between Side Ⅰ and Side Ⅱ. M. Emin reported the same pattern [10].

Figure 6. Water surface profiles on Side I, Side II, and Side III with a side weir width of 20 cm and height of 15 cm at a discharge of 25 L/s.

For a more accurate study on the entrance effect of the side weir on the Water Surface Profile (WSP) for Side I; a comparative analysis conducted using different widths but the same height (15 cm) at a discharge rate of 25 L/s is presented through Figure 7, Figure 8, Figure 9 and Figure 10.

Figure 7. Water surface profile on Side Ⅰ with a side weir width of 20 cm and height of 15 cm at a discharge of 25 L/s.
Figure 8. Water surface profile on Side Ⅰ with a side weir width of 30 cm and height of 15 cm at a discharge of 25 L/s.
Figure 9. Water surface profile on Side Ⅰ with a side weir width of 40 cm and height of 15 cm at a discharge of 25 L/s.
Figure 10. Water surface profile on Side Ⅰ with a side weir width of 47 cm and height of 15 cm at a discharge of 25 L/s.

According to Figure 7, Figure 8, Figure 9 and Figure 10, the water depth upstream of the main channel started to decrease as it approached the upstream end of the weir crest and then gradually increased at the weir crest section. In other words, the water surface profile exhibited a backwater curve along the length of the weir crest. The water depth remained relatively stable downstream of the main channel within a certain range from the downstream end of the weir crest. Additionally, there was a higher water depth downstream of the main channel compared to that upstream of the main channel. Furthermore, an increase in the width of the side weir led to a gradual reduction in fluctuations on its water surface.

5.2. Velocity Distribution

The law of flow velocity distribution near the side weir is the focus of research and analysis, so the simulated and measured values of flow velocity near the side weir were compared and analyzed. Take the discharge of 25 L/s, the height of 15 cm, and the width of 30 cm of the side weir as an example to illustrate. Figure 11 shows the measured and simulated velocity distribution in the x-direction of cross-section ④. As can be seen from Figure 11, the diagrams of the measured and simulated velocity distribution were relatively consistent, and the maximum absolute relative error between the measured and simulated values at the same measurement point was 9.37%, and the average absolute relative error was 3.97%, which indicated a satisfactory agreement between the experimental and simulated results.

Figure 11. Velocity distribution in the x-direction of section ④: when the discharge is 25 L/s, the height of the side weir is 15 cm and the width of the side weir is 30 cm. (a) Measured velocity distribution; (b) Simulated velocity distribution.

From Figure 11, it can be seen that the flow velocity gradually increased from the bottom of the channel towards the water surface in the Z-direction, and the flow velocity gradually increased from Side Ⅲ to Side Ⅰ in the Y-direction. The maximum flow velocity occurred near the weir crest.

Figure 12 shows the distribution of flow velocity at different depths (z/P = 0.3, z/P = 0.8, z/P = 1.6) with a side weir width of 30 cm and height of 15 cm at a discharge of 25 L/s. The water flow line began to bend at a certain point upstream of the main channel, and the closer it was to the upstream end of the weir crest, the greater the curvature. The maximum curvature occurred at the downstream end of the weir crest. The flow patterns at the bottom, near the side weir crest, and above the side weir crest were significantly different. There was a reverse flow at the bottom of the main channel, where the forward and reverse flows intersect, resulting in a detention zone. The maximum flow velocity at the bottom layer occurred at the upstream end of the side weir crest. When the location of water flow approached the weir crest, the maximum flow velocity occurred at the upstream end of the weir crest. The maximum flow velocity on the water surface occurred at the downstream end of the weir crest. As the water depth decreased, the position of the maximum flow velocity gradually moved from the upstream end of the side weir to the downstream end of the side weir.

Figure 12. Distribution of flow velocity at different depths with a side weir width of 30 cm and height of 15 cm at a discharge of 25 L/s. (a) z/P = 0.3; (b) z/P = 0.8; (c) z/P = 1.6.

5.3. Side Channel Pressure Distribution

When water flowed through the side weir, an upstream water level was formed, resulting in a pressure zone at the junction with the side channel. This pressure zone led to increased water pressure on the floor of the side channel, which affected its stability and durability. In small channels or fields where erosion resistance is weak, excessive pressure can cause scour holes. Therefore, analyzing the pressure distribution in the side channel is necessary to select an appropriate height and width for the side weir that effectively reduces its impact on the bottom plate.

To investigate the impact of side weir width on hydraulic characteristics, pressure data was collected at a discharge rate of 25 L/s for side weirs with heights of 20 cm and widths ranging from 20 cm to 47 cm. The pressure distribution map was drawn, as shown in Figure 13.

Figure 13. Comparison of pressure distribution on the bottom plate of the side channel with different widths of side weirs when the discharge is 25 L/s and the height of side weirs is 20 cm. (aP = 20 cm, b = 20 cm; (bP = 20 cm, b = 30 cm; (cP = 20 cm, b = 40 cm; (dP = 20 cm, b = 47 cm.

As can be seen from Figure 13, the pressure at the bottom of the side channel decreased as the width of the side weir increased. This uneven distribution of water flow on the weir was caused by the sharp bending of water flow lines and the influence of centrifugal inertia force over a short period. After passing through the side weir, the water flow became symmetrically distributed with respect to the axis of the side channel, leaning towards the right bank at a certain distance. As we increased the width of the side weir, we noticed that its position gradually approached the side weir and maximum pressure decreased at this location where the water tongue formed due to flowing through it (Figure 13). For a constant height (20 cm) but varying widths (20 cm, 30 cm, 40 cm, and 47 cm), we measured maximum pressures at these positions as follows: 103,713 Pa, 103,558 Pa, 103,324 Pa, and 103,280 Pa, respectively. Consequently, increasing width reduced the impact on the side channel from water flowing through it while changing pressure distribution from concentration to dispersion in a vertical direction. In the practical application of side weirs, appropriate height should be selected based on the bottom plate’s capacity to withstand the pressure exerted by flowing water within channels.

To investigate how height affects the hydraulic characteristics of rectangular side weirs further (Figure 14), we extracted pressures on bottom plates when discharge was fixed at 25 L/s while varying heights were set as follows: 7 cm, 10 cm, 15 cm, and 20 cm, respectively.

Figure 14. Comparison of pressure distribution on the bottom plate of the side channel with different heights of side weirs when discharge is 25 L/s and the width of side weirs is 20 cm. (aP = 7 cm, b = 20 cm; (bP = 10 cm, b = 20 cm; (cP = 15 cm, b = 20 cm; (dP = 20 cm, b = 20 cm.

As shown in Figure 14, when the width of the side weir was constant, the pressure at the bottom of the side channel increased with the height of the side weir. As the height of the side weir increased, the water tongue formed by flow through the side weir gradually moved away from it in a downstream direction. In terms of vertical water flow, as the height of the side weir increased, the position of maximum pressure at which the water tongue falls shifted closer to the axis of the side channel from its right bank. Moreover, an increase in height resulted in higher maximum pressure at this falling point. For a constant width (20 cm) and varying heights (7 cm, 10 cm, 15 cm, and 20 cm), corresponding maximum pressures at this landing point were measured as 102,422 Pa, 102,700 Pa, 103,375 Pa, and 103,766 Pa, respectively. Consequently, increasing width led to a greater impact on both flow through and pressure distribution within the side channel; transforming it from scattered to concentrated along its lengthwise direction. Therefore, when applying such weirs practically one should select an appropriate width based on what pressure can be sustained by their respective channel bottom plates.

5.4. Discharge Coefficient

Based on dimensionless analysis, the influencing parameters of the discharge coefficient were obtained. To study the effect of parameters Fr1b/h1, and P/h1, discharge coefficient values were plotted against Fr1b/h1, and P/h1, shown in Figure 15, Figure 16 and Figure 17. The discharge coefficient decreased as parameters Fr1 and b/h1 increased. The discharge coefficient increased as parameter P/h1 increased. As Uyumaz and Muslu reported in a previous study, the variation of the discharge coefficient with respect to the Froude number showed a second-degree curve for a subcritical regime [4].

Figure 15. Variation of discharge coefficient values against Froude number.
Figure 16. Variation of discharge coefficient values against the percentage of the side weir width to the upstream flow depth over the side weir.
Figure 17. Variation of discharge coefficient values against the percentage of the side weir height to the upstream flow depth over the side weir.

Quantitative analysis between discharge coefficient values and parameters Fr1b/h1, and P/h1 was conducted using data analysis software (IBM SPSS Statistics 19). The various coefficients obtained are shown in Table 3.

ModelUnstandardized CoefficientsStandardized CoefficientstSig
BStd. ErrorBeta (β)
Constant−1.2940.155−8.3690.000
Fr13.4300.2863.40112.0130.000
b/h1−0.0040.004−0.045−0.9440.348
P/h12.4010.1674.06414.3940.000
Table 3. Coefficient.

The value of t and Sig are the significance results of the independent variable, and the value of Sig corresponding to the value of t is less than 0.05, indicating that the independent variable has a significant impact on the dependent variable. Therefore, the values of Sig corresponding to the parameters Fr1 and P/h1 were less than 0.05, indicating that the parameters Fr1 and P/h1 have a significant impact on the discharge coefficient. On the contrary, the parameter b/h1 has less impact on the discharge coefficient. Therefore, quantitative analysis between discharge coefficient values and parameters Fr1, and P/h1 was conducted using data analysis software by removing factor b/h1. The model summary, ANOVA, and coefficient obtained are shown respectively in Table 4, Table 5 and Table 6. R and adjusted R square in Table 4 were approaching 1, which indicated the goodness of fit of the regression model was high. The value of Sig corresponding to the value of F in Table 5 was less than 0.05, which indicated that the regression equation was useful. The values of Sig corresponding to the parameters Fr1 and P/h1 in Table 6 were less than 0.05, indicating that the parameters Fr1 and P/h1 have a significant impact on the discharge coefficient.

ModelRR SquareAdjusted R SquareStd. Error of the Estimate
10.913 a0.8330.8290.03232
Table 4. Model Summary b. Note: a. Predictors:(Constant), Fr1P/h1b. Discharge coefficient.
ModelSum of SquaresdfMean SquareFSig
1Regression0.40220.201192.5450.000 a
Residual0.080770.001
Total0.48379
Table 5. ANOVA b. Note: a. Predictors:(Constant), Fr1P/h1b. Discharge coefficient.
ModelUnstandardized CoefficientsStandardized CoefficientstSig
BStd. ErrorBeta (β)
Constant−1.3260.151−8.7960.000
Fr13.4790.2813.44912.3960.000
P/h12.4270.1644.10814.7650.000
Table 6. Coefficient a. Note: a. Predictors:(Constant), Fr1P/h1.

Based on the above analysis, the flow coefficient formula has been obtained, shown as follows:

Discharge formula were obtained by substituting Equation (15) into Equation (12), as shown in Equation (16).

where Q ∈ [0.006, 0.030], m3/s; b ∈ [0.20, 0.47], m; P ∈ [0.07, 0.20], m.

Figure 18 showed the measured discharge coefficient values with those calculated from discharge formulas in Table 3. The scatter of the data with respect to perfect line was limited to ±10%.

Figure 18. Comparison of the measured discharge coefficient values with those calculated from discharge formulas in Table 3.

6. Discussions

Determining water surface profile near the side weir in the main channel is one of the tasks of hydraulic calculation for side weirs. As the water flows through the side weir, discharge in the main channel is gradually decreasing, namely dQ/ds<0. According to the Equation (17) derived from Qimo Chen [3], it can be inferred that the value of 𝑑ℎ/𝑑𝑠 is greater than zero in subcritical flow (Fr < 1), that is, the water surface profile near the side weir in the main channel is a backwater curve. Due to the side weir entrance effect at the upstream end, water surface profiles drop slightly at the upstream end of the side weir crest, as EI-Khashab [28] and Emiroglu et al. [29] reported in previous experimental studies.

In this study, the water surface profile exhibited a backwater curve along the length of the weir crest. Therefore, during side weir application, it is crucial to ensure that downstream water levels do not exceed the highest water level of the channel.

The head on the weir is one of the important factors that flow over side weirs depends on. At the same time, the head depends on the water surface profile near the side weir in the main channel. Therefore, further research on the quantitative analysis of water surface profile needs to be conducted. Mohamed Khorchani proposed a new approach based on the video monitoring concept to measure the free surface of flow over side weirs. It points out a new direction for future research [8].

The maximum flow velocity, a key parameter in assessing the efficiency of a weir, occurs at the upstream end of the weir crest, typically near the crest. This is attributed to the convergence of the flow as it approaches the crest, resulting in a significant increase in velocity. It was found that in this study the minimum flow velocity occurred at the bottom of the main channel away from the side weir. Under such conditions, the accumulation of sediments could lead to siltation, which in turn can affect the accuracy of flow measurement through side weirs. This is because the presence of sediments can alter the flow patterns and cause errors in the measurement. Therefore, it becomes crucial to explore methods to optimize the selection of side weirs in order to minimize or eliminate the effects of sedimentation on flow measurement.

Pressure distribution plays a crucial role in ensuring structural safety for side weirs since small channels and field inlets have relatively limited pressure-bearing capacities. Therefore, it is important to select an appropriate geometrical parameter of rectangular side weirs based on their ability to withstand the pressure exerted on their bottom combined with pressure distribution data at the bottom of the side channel we have obtained in this study.

The discharge coefficient formula (Equation (15)), which incorporates Fr1 and P/h1, was derived based on dimensional analysis. However, it is worth noting that previous research has contradicted this formula by suggesting that the discharge coefficient solely depends on the Froude number. This conclusion can be observed in this study such as in Equations (18)–(23) in Table 7 of the manuscript [30,31,32,33,34,35], which clearly demonstrate the dependency of the discharge coefficient on the Froude number. In contrast, our derived discharge coefficient formula (Equation (15)) offers a more streamlined and simplified approach compared to Equation (25) [36] and Equation (29) [10]—making it easier to comprehend and apply—an advantageous feature particularly valuable in fluid dynamics where intricate calculations can be time-consuming. Furthermore, our derived discharge coefficient formula (Equation (15)) exhibits a broader application scope than that of Equation (24) [37] as shown in Table 8. Equation (26) [38] and Equation (27) [5] are specifically applicable under high flow discharge conditions. Conversely, our derived discharge coefficient formula (Equation (15)) is better suited for low-flow discharge conditions.

Table 7. Discharge coefficient formulas of rectangular side weirs presented in previous studies.
Discharge/(L·s−1)Width of Side Weir/cmHeight of Side Weir/cmNumber of Formula
10~1410~206~12(24)
35–10020~751~19(26), (27)
6~3020~477~20(15)
Table 8. Application scope of discharge coefficient formulas.

In addition to the factors studied in the paper, factors such as the sediment content in the flow, the bottom slope, and the cross-section shape of the channel also have a certain impact on the hydraulic characteristics of the side weir. Further numerical simulation methods can be used to study the hydraulic characteristics and the influencing factors of the side weir. Water measurement facilities generally require high accuracy of water measurement, the flow of sharp-crested side weirs is complex, and the water surface fluctuates greatly. While conducting numerical simulations, experimental research on prototype channels is necessary to ensure the reliability of the results and provide reference for the body design and optimization of side weirs in small channels and field inlets.

7. Conclusions

This paper presents a comprehensive study that encompasses both experimental and numerical simulation research on rectangular side weirs of varying heights and widths within rectangular channels. A thorough analysis of the experimental and numerical simulation results has been conducted, leading to the derivation of several notable conclusions:

  1. A comparative analysis was conducted on the measured and simulated values of water depth and flow velocity. Both of the maximum absolute relative errors were within 10%, which indicated that the numerical simulation of the side weir was feasible and effective.
  2. The water surface profile exhibited a backwater curve along the length of the weir crest. The side weir entrance effect occurred only between Side Ⅰ and Side Ⅱ. This indicates that flow patterns and associated hydraulic forces at the weir entrance play a crucial role in determining water level distribution along the weir crest.
  3. The maximum flow velocity of the cross-section at the upstream end of the weir crest occurred near the weir crest, while the minimum flow velocity occurred at the bottom of the main channel away from the side weir. As the water depth decreased, the position of the maximum flow velocity gradually moved from the upstream end of the side weir to the downstream end of the side weir.
  4. When the height of the side weir remains constant, an increase in the width of the side weir leads to a decrease in pressure at the bottom of the side channel. Conversely, when the width of the side weir is kept constant, an increase in its height results in an increase in pressure at the bottom of the side channel. Therefore, during practical applications involving side weirs, it is crucial to select an appropriate weir width based on the maximum pressure that can be sustained by the channel’s bottom plate.
  5. The discharge coefficient was found to depend on the upstream Froude number Fr1 and the percentage of the side weir height to the upstream flow depth over the side weir P/h1. The relationship between the discharge coefficient and parameters Fr1 and P/h1 was obtained using multiple regression analysis, which was of linear form and provided an easy means to estimate the discharge coefficient. The discharge formula is of high accuracy with relative errors within 10%, which met the water measurement accuracy requirements of small channels in irrigation areas.

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Nozzle Scour

Study on the Sand-Scouring Characteristics of Pulsed Submerged Jets Based on Experiments and Numerical Methods

실험과 수치 해석을 기반으로 한 펄스 잠수 제트의 모래 침식 특성 연구

Hongliang Wang, Xuanwen Jia,Chuan Wang, Bo Hu, Weidong Cao, Shanshan Li, Hui Wang

Abstract


Water-jet-scouring technology finds extensive applications in various fields, including marine engineering. In this study, the pulse characteristics are introduced on the basis of jet-scouring research, and the sand-scouring characteristics of a pulsed jet under different Reynolds numbers and the impact distances are deeply investigated using Flow-3D v11.2. The primary emphasis is on the comprehensive analysis of the unsteady flow structure within the scouring process, the impulse characteristics, and the geometric properties of the resulting scouring pit. The results show that both the radius and depth of the scour pit show a good linear correlation with the jet-flow rate. The concentration of suspended sediment showed an increasing and then decreasing trend with impinging distance. The study not only helps to enrich the traditional theory of jet scouring, but also provides useful guidance for engineering applications, which have certain theoretical and practical significance.

Keywords


pulsed jet; turbulent structure; scouring characteristics

1. Introduction


Water-jet-scouring technology is widely used in marine engineering and its related ancillary fields, such as in the maintenance and repair of marine structures, extraction of deep-sea resources, dredging works, seabed geological research, and cleaning and maintenance of ships. The jet flow establishes a velocity shear layer at its boundary, leading to the destabilization and subsequent generation of vortices. These vortices undergo continuous deformation, rupture, merging, and evolution into turbulence during their movement. Consequently, they entrain surrounding fluid into the jet region, facilitating the transfer of momentum, heat, and mass between the jet and its ambient environment [1,2,3]. Therefore, numerous scholars have carried out detailed studies on the scouring characteristics associated with jets. Chatterjee et al. [4] investigated the local scouring and sediment-transport phenomena due to the formation of horizontal jets during the opening of sluice gates based on experiments, and successfully established empirical expressions for the correlation between the time of reaching the equilibrium stage, the maximum depth of scouring, and the peak of the dune. The important role of jet-diffusion properties in the scouring process was also emphasized. Hoffmans [5] calculated the equilibrium scour process induced using a horizontal jet in the absence of a streambed and used experiments to verify the accuracy of the equations for jet-scour depths in the relevant literature. Luo et al. [6] investigated the induction mechanism of scour in planar jets through particle-image velocimetry (PIV). It was found that the initial stage of scour was dominated by wall shear, while the later stages of the scour process were mainly influenced by the turbulent vortex. Canepa et al. [7] investigated the scour characteristics of gas-doped water jets and found that gas-doped jets significantly reduce the scour depth if the velocity of the mixture is used as a reference.
Pulsed jets introduce pulsation, resulting in a water-hammer effect, as well as increased diffusion and coil suction rates. These factors contribute to a more intricate interaction between the pulsed jet and the adjacent wall. The process of generation, development and evolution of its internal vortex structure as well as the interaction between the vortex structure and the surrounding ambient fluid and solid wall have changed significantly [8,9]. At this juncture, researchers in this domain have undertaken investigations centered on the utilization of pulsed jets. Coussement et al. [10] investigated the flow characteristics of a pulsed jet in a cross-flow environment based on Large Eddy Simulation (LES). A new approach to characterize mixing was introduced, which successfully explains and quantifies the complex mixing process between the pulsating jet and the ambient fluid. Bi et al. [11] investigated the thrust of a deformable body generated through a pulsed jet based on an axisymmetric immersed-boundary model. The numerical results show that in addition to the momentum flux of the jet, the jet acceleration is also an important source of thrust generation. Zhang et al. [12] studied the complex unsteady flow characteristics of a pulsed jet impinging on a rotating wall using numerical methods, and it was found that the impact pressure of the pulsed jet on the wall is greater than that of the continuous jet on the wall for a certain period of time when the water-hammer effect occurs. Rakhsha et al. [13] used experiments and numerical simulations to study the effect of pulsed jets on the flow and heat-transfer characteristics over a heated plane. It was found that the Nussell number increases with increasing pulse frequency and Reynolds number and decreases with increasing impinging distance. It is evident that existing studies predominantly center on the unsteady flow characteristics of pulsed jets and their properties related to heat and mass transfer. Conversely, there is a noticeable dearth of research concerning the scouring attributes of pulsed jets in the available literature.
The pulsed submerged impinging jet represents a complex jet flow with a significant engineering application background and substantial theoretical research value. Exploring the unsteady hydraulic characteristics of pulsed jets can enhance classical impinging jet theory, deepen our comprehension of the jet–wall interaction mechanism, and establish a scientific foundation for addressing engineering-application challenges. Therefore, this paper introduces the pulse characteristics into the impinging jet, and, based on the Flow-3D software, the sand-scouring characteristics of the impinging jet under different Reynolds numbers and impinging distances are deeply investigated. The surface geometry of the scour pit is characterized while obtaining the pulsation characteristics of the unsteady flow structure during sand scouring. This study not only offers a foundation for implementing flow control and enhancing the understanding of unsteady flow characteristics but also furnishes theoretical backing for predicting impact pressure and impact pit formation.

2. Modeling and Numerical Methods

2.1. Model Building

The geometric model consists of a jet pipe, a body of water, a baffle, and a sand bed, as shown in Figure 1. The inner diameter D of the jet pipe is 20 mm, and the length L is set to 50D to ensure that the turbulence inside the pipe is fully developed. H represents the impinging height, and the initial water height (Hw) is 1600 mm. Baffles positioned on both sides serve to maintain a constant water level. The length Ls and thickness Hs of the sand bed are 5000 mm and 160 mm, respectively. It is worth stating that the sand bed is composed of non-cohesive sand. The median grain size dm of the sand is 0.77 mm, the specific gravity Δ is 1.65, and the particle gradation σg is 1.21.

Figure 1. Geometric modeling for sand scouring.

2.2. Numerical Models

In fluid mechanics, the continuity and momentum equations are the basic governing equations [14]:

where uvw denote the velocity of the fluid in the xyz direction, respectively; AxAyAz denote the area fraction of the fluid in the xyz direction, respectively; VF denotes the volume fraction; P is the pressure exerted on the fluid micrometric elements; GxGyGz are the gravitational acceleration in the xyz direction, respectively; and fxfyfz are the viscous forces in the xyz direction, respectively.

In numerical simulations, the selection of a turbulence model significantly influences the accuracy of the calculations. Hence, it is imperative to choose an appropriate turbulence model. Given that this paper primarily deals with fully developed circular tube turbulence, which entails velocity and momentum coupling among fluids and features substantial time and spatial scales in the non-constant flow, the RNG kε turbulence model [15,16,17] has been chosen for the conclusive numerical simulation work. The RNG model takes into account the effect of eddies on turbulence and improves the accuracy of vortex-flow prediction [18]. Its equations are as follows:

where vt is the eddy viscosity coefficient; μ is the kinetic viscosity coefficient; the empirical constants cε1 and cε2 have values of 1.42 and 1.68; c3 = 0.012; η0 = 4.38; cμ = 0.085; and the values of Prandtl numbers αk and αε corresponding to the turbulent kinetic energy k and the dissipation rate ε are both 0.7194.

The Flow-3D software realizes an accurate description of the sediment movement with the help of an empirical equation model proposed by Mastbergen and Van den Berg [19]. The critical Shields number first needs to be calculated from the Soulsby–Whitehouse equation [20], which is given below:

where ρi is the sediment density, ρf is the fluid density, di is the sediment diameter, μf is the hydrodynamic viscosity, and ‖g‖ is the magnitude of gravitational acceleration.

Under the action of the jet, part of the deposited sediment will be disturbed to show a suspended state and it will continue to move under the carrying of the fluid. The uplifting velocities of entrained sediment ulift,i and usetting,i are calculated as follows:

where αi is the sediment carryover coefficient with a recommended value of 0.018 [19]; ns is the normal direction of the bed; and vf is the kinematic viscosity of the liquid.

2.3. Grid-Independent Analysis

It is well known that the number of the grid is closely related to the accuracy and cost of the numerical calculation. In order to investigate the optimal number of grids suitable for this numerical simulation, the scour depth Ht of the sand bed at H/D = 2 and inlet flow velocity Vb = 1.485 m/s is chosen as the monitoring parameter for the grid-independent analysis. Five sets of grid schemes with increasing numbers are set, and the results of the independence analysis are shown in Figure 2. From the figure, it can be seen that the depth of the scour pit Ht increases gradually with the encryption of the grid. When the grid is encrypted to Scheme 4, Ht almost no longer increases. It is considered that the number of meshes at this time can already meet the accuracy requirements of numerical calculations. Therefore, the grid number scheme in Scheme 4 is selected for the subsequent numerical simulation study, and the grid number is 43,825.

Figure 2. Grid-independent analysis.

2.4. Grid Delineation and Boundary Conditions

Within the Flow-3D software, a grid block is used that covers the entire 2D computational area as shown in Figure 1. Given the large aspect ratio of the jet pipe and the significant turbulent coupling between the fluid and sediment near the pipe outlet, grid refinement is implemented in the vicinity of the pipe outlet. The grid-encrypted area is mainly the area between the jet outlet and the sand bed, as shown in Figure 3. In addition, a mesh node is provided at the baffle on each side of the computational domain to ensure proper identification of the fluid boundary during numerical simulations. The upper boundary of the computational domain is defined as a velocity inlet, where the velocity magnitude is denoted as Vb, and the direction is oriented vertically downward. The lower boundary is the wall and no fluid or sediment flux is allowed. The two side boundaries are specified as pressure boundaries and the pressure is set to be 0 Pa. Based on the requirement of 2D numerical simulation, the boundaries of the front and rear sides are set as symmetric boundaries, both with one grid node. At the same time, the boundary-layer mesh near the pipe and the sand bed is encrypted accordingly. y+ is set at around 30 to ensure that the first grid nodes are in the turbulence core region, so as to ensure that the RNG kε turbulence model is perfectly adapted to the boundary conditions. Considering that the velocity strength and pressure gradient of the fluid around the baffle are small and it is not an observation area, the encryption of the boundary-layer grid is not performed for the time being.

Figure 3. Computational grid.

Numerical simulations are performed using the discrete control equations of the control volume method, with the diffusion term of the equations in the central difference format and the convection term in the second-order upwind format, and the equations are solved using a coupled algorithm. The standard wall equations are used, and the no-slip option in the wall shear boundary conditions is checked. In the non-stationary numerical simulation, the time step is set to 0.05 s. In order to ensure the accuracy of the numerical calculations, each time step is iterated 100 times, and the convergence accuracy is set to 10−5.

In this paper, the continuous jet is periodically truncated to form a blocking pulsed jet. The pulse period of its pulse velocity can be expressed as T = tj + t0 (tj and t0 are the jet time and truncation time, respectively, taking the value of 0.5 s), and the inlet flow rate of the jet pipe is Vb during the jet time period, while the inlet flow rate of the jet pipe is 0 during the truncation time period, as shown in Figure 4.

Figure 4. Velocity characteristics of the blocking pulsed jet.

3. Experimental Validation

To validate the accuracy of the numerical simulations, an experimental investigation of jet impingement on sediment is conducted. The experimental setup is shown in Figure 5. The parameters characterizing the sediment in the experiments are guaranteed to be the same as the settings in the numerical simulations. Specifically, non-cohesive sand is used with a median particle size dm of 0.77 mm, a specific gravity Δ of 1.65, and a particle gradation σg of 1.21. An angle plate is employed to control the impinging angle of the jet pipe, a COMS camera captures images of the pit, and a laser range finder is utilized for precise measurements of pit depth and dune height. In order to quantitatively describe the effect of jet impingement, the depth of the sand pit and the height of the dune are defined as d and h, respectively.

Figure 5. Schematic diagram of the experimental setup.

Figure 6 compares the stabilized morphology of the sand bed formed under the scouring of the jet for an impinging distance H/D of two in the numerical simulation and the experiment. The inlet flow velocities Vb of the jet pipe are 0.424 m/s, 0.955 m/s, and 1.485 m/s, respectively. As depicted in the figure, the ultimate scouring morphology of the sand bed, as obtained through numerical simulation, closely aligns with the experimental results. This alignment underscores the strong agreement between the numerical simulation and the experimental data. Nevertheless, it must be recognized that the final scour depths of the numerical simulations are all slightly smaller than the experimental values under the same conditions. The possible reason for this is the wall effect, i.e., the porosity of the actual sand bed is not homogeneous, with the upper sand layer being slightly more porous [21], whereas the porosity of the sand bed in the numerical simulation strictly follows the set value. Given that the accuracy of numerical calculations is subject to various influencing factors, and considering that the numerical solution inherently involves an approximation process, the numerical methods employed in this study can be deemed both accurate and dependable.

Figure 6. Comparison of sand-scouring experiment and numerical simulation: (aVb = 0.424 m/s; (bVb = 0.955 m/s; (cVb = 1.485 m/s.

4. Results and Discussion

There are many factors that affect the performance of jet scouring, such as the shape of the nozzle, the size of the nozzle, the inlet flow rate of the jet pipe, the impinging distance, and the sediment parameters. Changes in any one of these factors can have a large effect on the parameters that measure the scouring performance of the jet, such as the depth of the scouring pit |ymin|, the height of the dune ymax, the radius of the scouring pit R. In this paper, the effects of the inlet velocity Vb and impinging distance H/D on the scouring performance of the jet pipe are investigated. Seven working conditions with inlet velocity Vb of 0.424 m/s, 0.690 m/s, 0.955 m/s, 1.220 m/s, 1.485 m/s, 1.751 m/s and 2.016 m/s are calculated for different impinging distances H/D (H/D = 2, 4, 6 and 8). The corresponding Reynolds numbers Re are 8404, 13,657, 18,910, 24,162, 29,415, 34,667, and 39,920, respectively.

4.1. Characterization of Pit at Different Impinging Distances

After the jet impinges on the sand bed for a sustained period of time, the shape of the sand bed will no longer change and remain stable. Figure 7 shows the stable bed morphology formed by the jet impinging on the sand bed with different velocities Vb, and at different impinging distances H/D. The x-axis is at the axial position of the jet pipe, and the y-axis is the initial horizontal plane of the sand bed. As can be seen from the figure, under the condition of Vb = 0.424 m/s, the pit depths |ymin| corresponding to impinging distances H/D of two and four are basically equal. However, when H/D is increased to six, |ymin| becomes significantly smaller, and when H/D is eight, |ymin| increases again. Under the Vb = 0.690 m/s condition, the effect of H/D on the scour pit depth |ymin| is small, and its size basically stays around 3.5 cm. Under the Vb = 0.955 m/s condition, the pit depth corresponding to H/D = eight is slightly smaller than the pit depths at other impinging distances, and the magnitude of |ymin| is basically maintained near 4.6 cm. Under the Vb = 1.220 m/s condition, the change of the scouring pit depth |ymin| with the impinging distance H/D starts to be gradually significant, especially the scouring pit depth |ymin| which decreases by about 1.7 cm when the size of H/D increases from two to six. Under the condition of Vb = 1.220 m/s, the larger the H/D, the smaller the pit depth |ymin|, especially when the H/D is eight, the pit depth is obviously larger than the pit depth at other impinging distances. The corresponding pit depths |ymin| for Vb of 1.751 m/s and 2.016 m/s remain basically unchanged. From the above analysis, it can be seen that under the same Reynolds number conditions to some extent the impinging distance has a very limited effect on the depth of the pit |ymin|. When the impinging distance increases, the depth of the pit begins to decrease. This can be attributed to the fact that the increased distance results in the jet encountering the initial static water resistance over a longer duration, leading to a greater dissipation of kinetic energy and a subsequent reduction in the impinging force of the jet.

Figure 7. Pit characteristics at different impinging distances: (aVb = 0.424 m/s; (bVb = 0.690 m/s; (cVb = 0.955 m/s; (dVb = 1.220 m/s; (eVb = 1.485 m/s; (fVb = 1.751 m/s; (gVb = 2.016 m/s.

The depth of the scouring pit serves as a critical parameter for assessing the impact of jet impingement on sand beds, just as the height of the dune represents a key indicator for evaluating the effectiveness of this process. In Figure 7a, it can be seen that the dune height ymax increases synchronously with the increase of the impinging distance H/D at Vb = 0.424 m/s. When Vb ≥ 0.955 m/s, the dune height ymax no longer grows significantly with the increase of impinging distance H/D. To further explore the relationship between dune height and impinging distance, Figure 8 is plotted with the impinging distance as the horizontal coordinate and the dune heights on either side as the vertical coordinate. From the figure, it can be seen that when 0.424 m/s ≤ Vb ≤ 1.485 m/s, the dune height ymax increases with the increase of the impinging distance H/D, and the dune height ymax starts to decrease with the increase of the impinging distance H/D when Vb > 1.485 m/s. The reason behind the aforementioned phenomenon is that when the inlet velocity Vb of the jet pipe is low, suspended sediment tends to displace towards the sides of the dune, causing some of the sediment to accumulate on the dune and thereby increase its height. When Vb ≥ 1.485 m/s, due to the enhanced impact force, most of the suspended sediment no longer moves and accumulates near the dunes and sand pits, and it starts to move on the outside of the dunes, causing the dune height to decrease.

Figure 8. Variation in the height of dunes on either side of the scour pit with Vb: (a) left; (b) right.

In order to clarify the relationship between the pit radius R and the impinging distance H/D, the relationship is given in Figure 9. From the figure, it can be seen that when 0.424 ≤ Vb ≤ 0.690, the increase of impinging distance H/D has basically no effect on the radius R of the pit, and its magnitude always stays near 13 cm. As the inlet velocity Vb of the jet pipe increases (1.220 ≤ Vb ≤ 1.485), the impact of the pulsed jet intensifies. Consequently, the suspended sediment is propelled towards the sides of the sand pit; although, it has not reached the dune and the area beyond it. Instead, a substantial amount of suspended sediment settles within the sand pit on both sides. Simultaneously, as the impact distance increases, the reach of jet impact and the turbulence induced by the jet expand, leading to enhanced sediment transport on both sides of the sand pit. This ultimately results in a reduction in the radius of the scouring pit as the impinging distance increases.

Figure 9. Relationship between pit size and impinging distance.

4.2. Characterization of Piting at Different Reynolds Numbers

Figure 10 depicts the stabilized morphology of the sand pit resulting from the influence of jets with varying Reynolds numbers. Under the conditions of H/D = two and four, the inlet velocity Vb of the jet pipe is 0.424 m/s and 0.690 m/s, and the depth of the pit |ymin| is basically equal, which indicates that the impact of the jet on the sand bed at this time is small, and the sediment is only transported and circulated in the sand pit. When Vb ≥ 0.955, the depth of the pit |ymin| increases significantly with the increase of Vb. Under the condition of H/D = 6, the depth of the pit, denoted as |ymin|, ceases to remain constant when Vb is less than or equal to 0.690 m/s. However, the disparity between the two measurements remains relatively small, suggesting that the impact force and turbulence of the jet are already capable of transporting sediment from the bottom of the pit to its flanks when Vb ≤ 0.690 m/s. In the H/D = 8 condition, due to the impinging distance H/D is larger, and when the velocity of the jet pipe is small (Vb ≤ 0.690 m/s), the kinetic energy of the jet is continuously exchanged with the static water body and then reduced, making its impact force reduce, and the sediment can only be transported and circulated at the bottom of the sand pit. To further investigate the effect of the Reynolds number of the jet on the depth of the pit |ymin|, Figure 11 is plotted with the jet velocity Vb as the horizontal coordinate and the depth of the pit |ymin| as the vertical coordinate. From the figure, it is evident that there exists a strong linear relationship between the depth of the scouring pit and the jet velocity. The data points in the figure can be fitted to establish the following relationship between the depth of the scouring pit and the jet velocity:

Figure 10. Pit characteristics at different Reynolds numbers: (aH/D = 2; (bH/D = 4; (cH/D = 6; (dH/D = 8.
Figure 11. Linear relationship between scouring-pit depth and jet velocity.

4.3. Characterization of Pits with Different Impinging Times

Figure 12 illustrates the deformation of the sand bed caused by the impact of the pulsed jet over a time range from 0.75 s to 3.5 s (with intervals of 0.25 s). When the jet velocity Vb is 0.424 m/s, within the initial 0.75 s of jet initiation, the impact of the pulsed jet leads to noticeable deformation of the sand pit and dune, with their fundamental shapes taking form. The depth of the pit, denoted as |ymin|, continuously increases from 0.75 s to 2 s, eventually stabilizing around 2.75 s. By the onset of the pulsed jet, the dune has already assumed a fundamental profile, and its maximum height, represented as ymax, exhibits minimal variation over time, remaining relatively constant.

Figure 12. Changes in time scales of pits: (aVb = 0.424 m/s; (bVb = 0.690 m/s; (cVb = 0.955 m/s; (dVb = 1.220 m/s; (eVb = 1.485 m/s; (fVb = 1.751 m/s; (gVb = 2.016 m/s.

5. Conclusions

In this paper, a numerical computational study is conducted to examine the characteristics of sand-bed impingement using obstructing pulsed jets. A comprehensive analysis is undertaken, encompassing impingement-pit depth, dune height, and impingement-pit radius. The following conclusions are drawn:

  1. Under consistent jet-velocity conditions, the impingement distance (H/D) has minimal impact on the depth of the scouring pit within the range of 2 ≤ H/D ≤ 6. However, beyond this range (H/D > 6), increased impingement distance leads to heightened jet-energy dissipation, resulting in a weakened impact force and a subsequent reduction in pit depth. Additionally, for lower jet velocities, impinging-distance variations have negligible effects on pit radius, while higher jet velocities induce a decrease in pit radius with an increase in impinging distance.
  2. The study establishes strong linear relationships between both the radius and depth of the scouring pit and the jet velocity. However, the relationship between dune height and pulsed-jet velocity is characterized by randomness and uncertainty. The dynamics of sediment transport contribute to the lack of symmetry in the stable configuration of the sand pit concerning the jet-pipe axis. Furthermore, the relationship between dune height and pulsed-jet velocity exhibits transient characteristics, highlighting the complex nature of these interactions.
  3. The numerical computational analysis emphasizes the transient characteristics of the sand-pit configuration due to sediment-transport dynamics. The stable state of the pit does not assume symmetry with the jet pipe as the axis, introducing a level of asymmetry in the system. This asymmetry is crucial in understanding the complex behavior of the sand-bed impingement. The findings underscore the need to consider dynamic and transient factors when studying the impact of obstructing pulsed jets on sand-bed characteristics.

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Omega-Liutex Method

Prediction of the Vortex Evolution and Influence Analysis of Rough Bed in a Hydraulic Jump with the Omega-Liutex Method

Omega-Luitex법을 이용한 수력점프 발생시 러프 베드의 와류 진화 예측 및 영향 분석

Cong Trieu Tran, Cong Ty Trinh

Abstract

The dissipation of energy downstream of hydropower projects is a significant issue. The hydraulic jump is exciting and widely applied in practice to dissipate energy. Many hydraulic jump characteristics have been studied, such as length of jump Lj and sequent flow depth y2. However, understanding the evolution of the vortex structure in the hydraulic jump shows a significant challenge. This study uses the RNG k-e turbulence model to simulate hydraulic jumps on the rough bed. The Omega-Liutex method is compared with Q-criterion for capturing vortex structure in the hydraulic jump. The formation, development, and shedding of the vortex structure at the rough bed in the hydraulic jumper are analyzed. The vortex forms and rapidly reduces strength on the rough bed, resulting in fast dissipation of energy. At the rough block rows 2nd and 3rd, the vortex forms a vortex rope that moves downstream and then breaks. The vortex-shedding region represents a significant energy attenuation of the flow. Therefore, the rough bed dissipates kinetic energy well. Adding reliability to the vortex determined by the Liutex method, the vorticity transport equation is used to compare the vorticity distribution with the Liutex distribution. The results show a further comprehension of the hydraulic jump phenomenon and its energy dissipation.

Keywords

flow-3D; hydraulic Jump; omega-liutex method; vortex breakdown

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Numerical Investigation of the Local Scour for Tripod Pile Foundation

Numerical Investigation of the Local Scour for Tripod Pile Foundation

Waqed H. Hassan Zahraa Mohammad Fadhe* Rifqa F. Thiab Karrar Mahdi
Civil Engineering Department, Faculty of Engineering, University of Warith Al-Anbiyaa, Kerbala 56001, Iraq
Civil Engineering Department, Faculty of Engineering, University of Kerbala, Kerbala 56001, Iraq
Corresponding Author Email: Waqed.hammed@uowa.edu.iq

OPEN ACCESS

Abstract: 

This work investigates numerically a local scour moves in irregular waves around tripods. It is constructed and proven to use the numerical model of the seabed-tripod-fluid with an RNG k turbulence model. The present numerical model then examines the flow velocity distribution and scour characteristics. After that, the suggested computational model Flow-3D is a useful tool for analyzing and forecasting the maximum scour development and the flow field in random waves around tripods. The scour values affecting the foundations of the tripod must be studied and calculated, as this phenomenon directly and negatively affects the structure of the structure and its design life. The lower diagonal braces and the main column act as blockages, increasing the flow accelerations underneath them.  This increases the number of particles that are moved, which in turn creates strong scouring in the area. The numerical model has a good agreement with the experimental model, with a maximum percentage of error of 10% between the experimental and numerical models. In addition, Based on dimensional analysis parameters, an empirical equation has been devised to forecast scour depth with flow depth, median size ratio, Keulegan-Carpenter (Kc), Froud number flow, and wave velocity that the results obtained in this research at various flow velocities and flow depths demonstrated that the maximum scour depth rate depended on wave height with rising velocities and decreasing particle sizes (d50) and the scour depth attains its steady-current value for Vw < 0.75. As the Froude number rises, the maximum scour depth will be large.

Keywords: 

local scour, tripod foundation, Flow-3D​, waves

1. Introduction

New energy sources have been used by mankind since they become industrialized. The main energy sources have traditionally been timber, coal, oil, and gas, but advances in the science of new energies, such as nuclear energy, have emerged [1, 2]. Clean and renewable energy such as offshore wind has grown significantly during the past few decades. There are numerous different types of foundations regarding offshore wind turbines (OWTs), comprising the tripod, jacket, gravity foundation, suction anchor (or bucket), and monopile [3, 4]. When the water depth is less than 30 meters, Offshore wind farms usually employ the monopile type [4]. Engineers must deal with the wind’s scouring phenomenon turbine foundations when planning and designing wind turbines for an offshore environment [5]. Waves and currents generate scour, this is the erosion of soil near a submerged foundation and at its location [6]. To predict the regional scour depth at a bridge pier, Jalal et al. [7-10] developed an original gene expression algorithm using artificial neural networks. Three monopiles, one main column, and several diagonal braces connecting the monopiles to the main column make up the tripod foundation, which has more complicated shapes than a single pile. The design of the foundation may have an impact on scour depth and scour development since the foundation’s form affects the flow field [11, 12]. Stahlmann [4] conducted several field investigations. He discovered that the main column is where the greatest scour depth occurred. Under the main column is where the maximum scour depth occurs in all experiments. The estimated findings show that higher wave heights correspond to higher flow velocities, indicating that a deeper scour depth is correlated with finer silt granularity [13] recommends as the design value for a single pile. These findings support the assertion that a tripod may cause the seabed to scour more severely than a single pile. The geography of the scour is significantly more influenced by the KC value (Keulegan–Carpenter number)

The capability of computer hardware and software has made computational fluid dynamics (CFD) quite popular to predict the behavior of fluid flow in industrial and environmental applications has increased significantly in recent years [14].

Finding an acceptable piece of land for the turbine’s construction and designing the turbine pile precisely for the local conditions are the biggest challenges. Another concern related to working in a marine environment is the effect of sea waves and currents on turbine piles and foundations. The earth surrounding the turbine’s pile is scoured by the waves, which also render the pile unstable.

In this research, the main objective is to investigate numerically a local scour around tripods in random waves. It is constructed and proven to use the tripod numerical model. The present numerical model is then used to examine the flow velocity distribution and scour characteristics.

2. Numerical Model

To simulate the scouring process around the tripod foundation, the CFD code Flow-3D was employed. By using the fractional area/volume method, it may highlight the intricate boundaries of the solution domain (FAVOR).

This model was tested and validated utilizing data derived experimentally from Schendel et al. [15] and Sumer and Fredsøe [6]. 200 runs were performed at different values of parameters.

2.1 Momentum equations

The incompressible viscous fluid motion is described by the three RANS equations listed below [16]:

(1)

\frac{\partial u}{\partial t}+\frac{1}{{{V}_{F}}}\left( u{{A}_{x}}\frac{\partial u}{\partial x}+v{{A}_{y}}\frac{\partial u}{\partial y}+w{{A}_{z}}\frac{\partial u}{\partial z} \right)=-\frac{1}{\rho }\frac{\partial p}{\partial x}+{{G}_{x}}+fx

(2)

\frac{\partial v}{\partial t}+\frac{1}{{{V}_{F}}}\left( u{{A}_{x}}\frac{\partial v}{\partial x}+v{{A}_{y}}\frac{\partial v}{\partial y}+w{{A}_{z}}\frac{\partial v}{\partial z} \right)=-\frac{1}{\rho }\frac{\partial p}{\partial y}+{{G}_{y}}+\text{f}y

 (3)

\frac{\partial w}{\partial t}+\frac{1}{{{V}_{F}}}\left( u{{A}_{x}}\frac{\partial w}{\partial x}+v{{A}_{y}}\frac{\partial w}{\partial y}+w{{A}_{z}}\frac{\partial w}{\partial z} \right)=-\frac{1}{\rho }\frac{\partial p}{\partial z}+{{G}_{z}}+\text{fz}

where, respectively, uv, and w represent the xy, and z flow velocity components; volume fraction (VF), area fraction (AiI=xyz), water density (f), viscous force (fi), and body force (Gi) are all used in the formula.

2.2 Model of turbulence

Several turbulence models would be combined to solve the momentum equations. A two-equation model of turbulence is the RNG k-model, which has a high efficiency and accuracy in computing the near-wall flow field. Therefore, the flow field surrounding tripods was captured using the RNG k-model.

2.3 Model of sediment scour

2.3.1 Induction and deposition

Eq. (4) can be used to determine the particle entrainment lift velocity [17].

(4)

{{u}_{lift,i}}={{\alpha }_{i}}{{n}_{s}}d_{*}^{0.3}{{\left( \theta -{{\theta }_{cr}} \right)}^{1.5}}\sqrt{\frac{\parallel g\parallel {{d}_{i}}\left( {{\rho }_{i}}-{{\rho }_{f}} \right)}{{{\rho }_{f}}}}

α𝛼  is the Induction parameter, ns the normal vector is parallel to the seafloor, and for the present numerical model, ns=(0,0,1), θ𝜃cr is the essential Shields variable, g is the accelerated by gravity, di is the size of the particles, ρi is species density in beds, and d The diameter of particles without dimensions; these values can be obtained in Eq. (5).

(5)

{{d}_{*}}={{d}_{i}}{{\left( \frac{\parallel g\parallel {{\rho }_{f}}\left( {{\rho }_{i}}-{{\rho }_{f}} \right)}{\mu _{f}^{2}} \right)}^{1/3}}

μ𝜇f is this equation a dynamic viscosity of the fluid. cr was determined from an equation based on Soulsby [18].

(6)

{{\theta }_{cr}}=\frac{0.3}{1+1.2{{d}_{*}}}+0.055\left[ 1-\text{exp}\left( -0.02{{d}_{*}} \right) \right]

The equation was used to determine how quickly sand particles set Eq. (7):

(7)

{{\mathbf{u}}_{\text{nsettling},i}}=\frac{{{v}_{f}}}{{{d}_{i}}}\left[ {{\left( {{10.36}^{2}}+1.049d_{*}^{3} \right)}^{0.5}}-10.36 \right]

vf  stands for fluid kinematic viscosity.

2.3.2 Transportation for bed loads

Van Rijn [19] states that the speed of bed load conveyance was determined as:

(8)

{{~}_{\text{bedload},i}}=\frac{{{q}_{b,i}}}{{{\delta }_{i}}{{c}_{b,i}}{{f}_{b}}}

fb  is the essential particle packing percentage, qbi is the bed load transportation rate, and cb, I the percentage of sand by volume i. These variables can be found in Eq. (9), Eq. (10), fbδ𝛿i the bed load thickness.

(9)

{{q}_{b,i}}=8{{\left[ \parallel g\parallel \left( \frac{{{\rho }_{i}}-{{\rho }_{f}}}{{{\rho }_{f}}} \right)d_{i}^{3} \right]}^{\frac{1}{2}}}

(10)

{{\delta }_{i}}=0.3d_{*}^{0.7}{{\left( \frac{\theta }{{{\theta }_{cr}}}-1 \right)}^{0.5}}{{d}_{i}}

In this paper, after the calibration of numerous trials, the selection of parameters for sediment scour is crucial. Maximum packing fraction is 0.64 with a shields number of 0.05, entrainment coefficient of 0.018, the mass density of 2650, bed load coefficient of 12, and entrainment coefficient of 0.01.

3. Model Setup

To investigate the scour characteristics near tripods in random waves, the seabed-tripod-fluid numerical model was created as shown in Figure 1. The tripod basis, a seabed, and fluid and porous medium were all components of the model. The seabed was 240 meters long, 40 meters wide, and three meters high. It had a median diameter of d50 and was composed of uniformly fine sand. The 2.5-meter main column diameter D. The base of the main column was three dimensions above the original seabed. The center of the seafloor was where the tripod was, 130 meters from the offshore and 110 meters from the onshore. To prevent wave reflection, the porous media were positioned above the seabed on the onshore side.

image013.png

Figure 1. An illustration of the numerical model for the seabed-tripod-fluid

3.1 Generation of meshes

Figure 2 displays the model’s mesh for the Flow-3D software grid. The current model made use of two different mesh types: global mesh grid and nested mesh grid. A mesh grid with the following measurements was created by the global hexahedra mesh grid: 240m length, 40m width, and 32m height. Around the tripod, a finer nested mesh grid was made, with dimensions of 0 to 32m on the z-axis, 10 to 30 m on the x-axis, and 25 to 15 m on the y-axis. This improved the calculation’s precision and mesh quality.

image014.png

Figure 2. The mesh block sketch

3.2 Conditional boundaries

To increase calculation efficiency, the top side, The model’s two x-z plane sides, as well as the symmetry boundaries, were all specified. For u, v, w=0, the bottom boundary wall was picked. The offshore end of the wave boundary was put upstream. For the wave border, random waves were generated using the wave spectrum from the Joint North Sea Wave Project (JONSWAP). Boundary conditions are shown in Figure 3.

image015.png

Figure 3. Boundary conditions of the typical problem

The wave spectrum peak enhancement factor (=3.3 for this work) and can be used to express the unidirectional JONSWAP frequency spectrum.

3.3 Mesh sensitivity

Before doing additional research into scour traits and scour depth forecasting, mesh sensitivity analysis is essential. Three different mesh grid sizes were selected for this section: Mesh 1 has a 0.45 by 0.45 nested fine mesh and a 0.6 by 0.6 global mesh size. Mesh 2 has a 0.4 global mesh size and a 0.35 nested fine mesh size, while Mesh 3 has a 0.25 global mesh size and a nested fine mesh size of 0.15. Comparing the relative fine mesh size (such as Mesh 2 or Mesh 3) to the relatively coarse mesh size (such as Mesh 1), a larger scour depth was seen; this shows that a finer mesh size can more precisely represent the scouring and flow field action around a tripod. Significantly, a lower mesh size necessitates a time commitment and a more difficult computer configuration. Depending on the sensitivity of the mesh guideline utilized by Pang et al., when Mesh 2 is applied, the findings converge and the mesh size is independent [20]. In the next sections, scouring the area surrounding the tripod was calculated using Mesh 2 to ensure accuracy and reduce computation time. The working segment generates a total of 14, 800,324 cells.

3.4 Model validation

Comparisons between the predicted outcomes from the current model and to confirm that the current numerical model is accurate and suitably modified, experimental data from Sumer and Fredsøe [6] and Schendel et al. [15] were used. For the experimental results of Run 05, Run 15, and Run 22 from Sumer and Fredsøe [6], the experimental A9, A13, A17, A25, A26, and A27 results from Schendel et al. [15], and the numerical results from the current model are shown in Figure 4. The present model had d50=0.051cm, the height of the water wave(h)=10m, and wave velocity=0.854 m.s-1.

image016.png

Figure 4. Cell size effect

image017.png

Figure 5. Comparison of the present study’s maximum scour depth with that authored by Sumer and Fredsøe [6] and Schendel et al. [15]

According to Figure 5, the highest discrepancy between the numerical results and experimental data is about 10%, showing that overall, there is good agreement between them. The ability of the current numerical model to accurately depict the scour process and forecast the maximum scour depth (S) near foundations is demonstrated by this. Errors in the simulation were reduced by using the calibrated values of the parameter. Considering these results, a suggested simulated scouring utilizing a Flow-3D numerical model is confirmed as a superior way for precisely forecasting the maximum scour depth near a tripod foundation in random waves.

3.5 Dimensional analysis

The variables found in this study as having the greatest impacts, variables related to flow, fluid, bed sediment, flume shape, and duration all had an impact on local scouring depth (t). Hence, scour depth (S) can be seen as a function of these factors, shown as:

(11)

S=f\left(\rho, v, V, h, g, \rho s, d_{50}, \sigma g, V_w, D, d, T_v, t\right)

With the aid of dimensional analysis, the 14-dimensional parameters in Eq. (11) were reduced to 6 dimensionless variables using Buckingham’s -theorem. D, V, and were therefore set as repetition parameters and others as constants, allowing for the ignoring of their influence. Eq. (12) thus illustrates the relationship between the effect of the non-dimensional components on the depth of scour surrounding a tripod base.

(12)

\frac{S}{D}=f\left(\frac{h}{D}, \frac{d 50}{D}, \frac{V}{V W}, F r, K c\right)

where, SD𝑆𝐷 are scoured depth ratio, VVw𝑉𝑉𝑤 is flow wave velocity, d50D𝑑50𝐷 median size ratio, $Fr representstheFroudnumber,and𝑟𝑒𝑝𝑟𝑒𝑠𝑒𝑛𝑡𝑠𝑡ℎ𝑒𝐹𝑟𝑜𝑢𝑑𝑛𝑢𝑚𝑏𝑒𝑟,𝑎𝑛𝑑Kc$ is the Keulegan-Carpenter.

4. Result and Discussion

4.1 Development of scour

Similar to how the physical model was used, this numerical model was also used. The numerical model’s boundary conditions and other crucial variables that directly influence the outcomes were applied (flow depth, median particle size (d50), and wave velocity). After the initial 0-300 s, the scour rate reduced as the scour holes grew quickly. The scour depths steadied for about 1800 seconds before reaching an asymptotic value. The findings of scour depth with time are displayed in Figure 6.

4.2 Features of scour

Early on (t=400s), the scour hole began to appear beneath the main column and then began to extend along the diagonal bracing connecting to the wall-facing pile. Gradually, the geography of the scour; of these results is similar to the experimental observations of Stahlmann [4] and Aminoroayaie Yamini et al. [1]. As the waves reached the tripod, there was an enhanced flow acceleration underneath the main column and the lower diagonal braces as a result of the obstructing effects of the structural elements. More particles are mobilized and transported due to the enhanced near-bed flow velocity, it also increases bed shear stress, turbulence, and scour at the site. In comparison to a single pile, the main column and structural components of the tripod have a significant impact on the flow velocity distribution and, consequently, the scour process and morphology. The main column and seabed are separated by a gap, therefore the flow across the gap may aid in scouring. The scour hole first emerged beneath the main column and subsequently expanded along the lower structural components, both Aminoroayaie Yamini et al. [1] and Stahlmann [4] made this claim. Around the tripod, there are several different scour morphologies and the flow velocity distribution as shown in Figures 7 and 8.

image023.png

Figure 6. Results of scour depth with time

image024.png

image025.png

image026.png

image027.png

Figure 7. The sequence results of scour depth around tripod development (reached to steady state) simulation time

image028.png

image029.png

image030.png

image031.png

Figure 8. Random waves of flow velocity distribution around a tripod

4.3 Wave velocity’s (Vw) impact on scour depth

In this study’s section, we looked at how variations in wave current velocity affected the scouring depth. Bed scour pattern modification could result from an increase or decrease in waves. As a result, the backflow area produced within the pile would become stronger, which would increase the depth of the sediment scour. The quantity of current turbulence is the primary cause of the relationship between wave height and bed scour value. The current velocity has increased the extent to which the turbulence energy has changed and increased in strength now present. It should be mentioned that in this instance, the Jon swap spectrum random waves are chosen. The scour depth attains its steady-current value for Vw<0.75, Figure 9 (a) shows that effect. When (V) represents the mean velocity=0.5 m.s-1.

image032.png

(a)

image033.png

(b)

image034.png

(c)

image035.png

(d)

Figure 9Main effects on maximum scour depth (Smax) as a function of column diameter (D)

4.4 Impact of a median particle (d50) on scour depth

In this section of the study, we looked into how variations in particle size affected how the bed profile changed. The values of various particle diameters are defined in the numerical model for each run numerical modeling, and the conditions under which changes in particle diameter have an impact on the bed scour profile are derived. Based on Figure 9 (b), the findings of the numerical modeling show that as particle diameter increases the maximum scour depth caused by wave contact decreases. When (d50) is the diameter of Sediment (d50). The Shatt Al-Arab soil near Basra, Iraq, was used to produce a variety of varied diameters.

4.5 Impact of wave height and flow depth (h) on scour depth

One of the main elements affecting the scour profile brought on by the interaction of the wave and current with the piles of the wind turbines is the height of the wave surrounding the turbine pile causing more turbulence to develop there. The velocity towards the bottom and the bed both vary as the turbulence around the pile is increased, modifying the scour profile close to the pile. According to the results of the numerical modeling, the depth of scour will increase as water depth and wave height in random waves increase as shown in Figure 9 (c).

4.6 Froude number’s (Fr) impact on scour depth

No matter what the spacing ratio, the Figure 9 shows that the Froude number rises, and the maximum scour depth often rises as well increases in Figure 9 (d). Additionally, it is crucial to keep in mind that only a small portion of the findings regarding the spacing ratios with the smallest values. Due to the velocity acceleration in the presence of a larger Froude number, the range of edge scour downstream is greater than that of upstream. Moreover, the scouring phenomena occur in the region farthest from the tripod, perhaps as a result of the turbulence brought on by the collision of the tripod’s pile. Generally, as the Froude number rises, so does the deposition height and scour depth.

4.7 Keulegan-Carpenter (KC) number

The geography of the scour is significantly more influenced by the KC value. Greater KC causes a deeper equilibrium scour because an increase in KC lengthens the horseshoe vortex’s duration and intensifies it as shown in Figure 10.

The result can be attributed to the fact that wave superposition reduced the crucial KC for the initiation of the scour, particularly under small KC conditions. The primary variable in the equation used to calculate This is the depth of the scouring hole at the bed. The following expression is used to calculate the Keulegan-Carpenter number:

Kc=Vw∗TpD𝐾𝑐=𝑉𝑤∗𝑇𝑝𝐷                          (13)

where, the wave period is Tp and the wave velocity is shown by Vw.

image037.png

Figure 10. Relationship between the relative maximum scour depth and KC

5. Conclusion

(1) The existing seabed-tripod-fluid numerical model is capable of faithfully reproducing the scour process and the flow field around tripods, suggesting that it may be used to predict the scour around tripods in random waves.

(2) Their results obtained in this research at various flow velocities and flow depths demonstrated that the maximum scour depth rate depended on wave height with rising velocities and decreasing particle sizes (d50).

(3) A diagonal brace and the main column act as blockages, increasing the flow accelerations underneath them. This raises the magnitude of the disturbance and the shear stress on the seafloor, which in turn causes a greater number of particles to be mobilized and conveyed, as a result, causes more severe scour at the location.

(4) The Froude number and the scouring process are closely related. In general, as the Froude number rises, so does the maximum scour depth and scour range. The highest maximum scour depth always coincides with the bigger Froude number with the shortest spacing ratio.

Since the issue is that there aren’t many experiments or studies that are relevant to this subject, therefore we had to rely on the monopile criteria. Therefore, to gain a deeper knowledge of the scouring effect surrounding the tripod in random waves, further numerical research exploring numerous soil, foundation, and construction elements as well as upcoming physical model tests will be beneficial.

Nomenclature

CFDComputational fluid dynamics
FAVORFractional Area/Volume Obstacle Representation
VOFVolume of Fluid
RNGRenormalized Group
OWTsOffshore wind turbines
Greek Symbols
ε, ωDissipation rate of the turbulent kinetic energy, m2s-3
Subscripts
d50Median particle size
VfVolume fraction
GTTurbulent energy of buoyancy
KTTurbulent velocity
PTKinetic energy of the turbulence
ΑiInduction parameter
nsInduction parameter
ΘΘcrThe essential Shields variable
DiDiameter of sediment
dThe diameter of particles without dimensions
µfDynamic viscosity of the fluid
qb,iThe bed load transportation rate
Cs,iSand particle’s concentration of mass
DDiameter of pile
DfDiffusivity
DDiameter of main column
FrFroud number
KcKeulegan–Carpenter number
GAcceleration of gravity g
HFlow depth
VwWave Velocity
VMean Velocity
TpWave Period
SScour depth

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[15] Schendel, A., Welzel, M., Schlurmann, T., Hsu, T.W. (2020). Scour around a monopile induced by directionally spread irregular waves in combination with oblique currents. Coastal Engineering, 161: 103751. https://doi.org/10.1016/j.coastaleng.2020.103751

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Investigating effects of lateral inflow characteristics on main flow using numerical modeling

Investigating effects of lateral inflow characteristics on main flow using numerical modeling

수치모델링을 이용한 측면 유입특성이 본류에 미치는 영향 조사

Mohammad Raze Raeisi Dehkordi1*, Amir Hossein Yeganeh Mazhar1
, Farzaneh Kheradzare2
1– PhD. Student in the Department of Construction and Water Management, Science and Research Unit, Islamic Azad
University, Tehran, Iran
2– M.Sc. Graduate Water resource management, Department of Civil Engineering and Mechanics, Ghiaseddin Jamshid
Kashani University, Qazvin, Iran

  • Corresponding author: mohamadreza.raeisi.d@gmail.com

Keywords

Channel Confluence, Channel cross, sectional area, Cross channel angles, Modelling, Flow-3D

Abstract

Introduction

One of the key issues in river engineering is analyzing the flow properties at the intersection of natural rivers and canals. The flow of the side channel moves away from the intersection of the two channels as a result of the exchange of input force from the side channel with the main flow after coming into contact with it. One of the most evident properties of the flow in these sections is the development of a revolving region with low pressure and even negative pressure close to the inner wall of the side channel. One advantage of the whirling flow in this low-pressure region is that it gives the flow enough space to sediment, but it also increases flow speed near the channel’s bottom and outside wall by lowering the intersectional area of the flow. One of the most crucial considerations in the design of these intersections is minimizing sedimentation in the rotating region and scouring in the area above the shear plane.

Materials and methods:

The channel (flume) created in the laboratory based on Weber et al., (2001) model, was employed in the current investigation to confirm the validity and examine other study objectives. The main channel is 21. 95 meters long, while the side channel, which is at a 90-degree angle to the main channel, is 3. 66 meters long. The total downstream discharge is approximately 0. 17 m3/s, with the upstream velocities of the main channel being 0. 166 m/s and the side channel being 0. 5 m/s. In both channels, the flow depth and width are 0. 91 meters and 0. 296 meters, respectively. In this study, 6 various models’ angles of intersection between the main and side channels, inlet flow velocity, intersectional area, and side channel length have been examined. Models 2 and 3 have intersection angles of 60 and 30 degrees, respectively, and share the rest of their attributes with the fundamental model, or model number 1. Model 1 is the same as Weber’s experimental model. The length of the side channel in model 4 is different from model 1. The only difference between model 6 and the basic model is the side channel intake speed.

Results and Discussion

Analyzing the intersection angle The angle between the main channel and the side channel is investigated in this section of the findings. Models 1, 2, and 3 are assessed using the intersection angles of 90, 60, and 30 degrees, respectively. In some studies, the impact of the intersection angle has been examined, but in this study, three-dimensional investigation in transverse and longitudinal sections as well as the plan of the intersection is discussed, as can be observed from the literature review. Considering three models with intersection angles of 90, 60, and 30 degrees, the kinetic energy contours at the channel’s middle height can be obtained for each model. The channel with a 30-degree intersection angle (model 3) has the maximum kinetic energy in the flow. The channel with a 60-degree intersection has the minimum kinetic energy. As a result of the maximum deviation of the flow in the main channel caused by the flow of the side channel, the channel with a 90-degree intersection also has the maximum kinetic energy near the wall in front of the side channel.

Examining the side channel length In model 1, the side channel is 3. 66 meters long, whereas in model 4, it is 5. 52 meters long. This study aims to determine how changing the side channel’s length affects the flow pattern where two channels intersect. The kinetic energy contours were obtained for two states of the channel length, which are known to extend the lateral channel, increase the energy of the flow after the intersection, and shorten the length of the high-kinetic energy zone. When compared to model 1 with a shorter length of the side channel, the width of the flow separation zone is reduced by approximately 20%, which results in less flow sedimentation. Figure 12 illustrates the rotating zones in the flow separation area. The flow separation region’s length is essentially unchanged. Studying the intersection of the lateral channel After determining the lateral channel’s length, its width and, consequently, its intersectional area should be evaluated.

This section compares model 1 width of 0. 91 meters to model 5 width of 1. 40 meters. One of the most recent topics related to the intersection of the main and side channels is examining the intersection of the side channel. In model 5, the side channel’s flow rate has also increased due to an increase in the width or intersection of the channel. The flow rate through the intersection and the momentum of the flow from the side channel and the main channel increase when the side channel flow rate rises. The findings indicate that when flow width and side channel flow rise, energy increases after the inlet.

Investigating the value of inlet speed in the side channel Unlike the preceding sections, which were all concerned with the channel geometry, the inlet velocity in the side channel is one of the hydraulic parameters of the flow. In this section, models 1 and 6 with inlet velocities of the side channel of 0. 5 and 0. 75 m/s are evaluated. According to the modeling, the flow is somewhat horst before and immediately on the intersection of the flow level, but it undergoes a substantial prolapse just after the intersection. Model 6 has a larger volume and height of flow, but a smaller and softer prolapse after the intersection.

Conclusion

Some hydraulic and geometric properties of the intersection of channels have been examined using Flow-3D software. The RNG turbulence model was used for three-dimensional modeling. Some of the results are listed below. The flow is uniform upstream of the main and minor channels and only slightly becomes horst at the intersection. The analysis of the lengthening of the side channel revealed a 20% reduction in the separation zone’s width and a considerable reduction in the kinetic energy at the intersection. The input flow rate of this channel to the intersection increases with the speed and width of the side channel, which accounts for the local drop in the width of the main channel flow.

References

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Estimating maximum initial wave amplitude of subaerial landslide tsunamis: A three-dimensional modelling approach

Estimating maximum initial wave amplitude of subaerial landslide tsunamis: A three-dimensional modelling approach

해저 산사태 쓰나미의 최대 초기 파동 진폭 추정: 3차원 모델링 접근법

Ramtin Sabeti a, Mohammad Heidarzadeh ab

aDepartment of Architecture and Civil Engineering, University of Bath, Bath BA27AY, UK
bHydroCoast Consulting Engineers Ltd, Bath, UK

https://doi.org/10.1016/j.ocemod.2024.102360

Highlights

  • •Landslide travel distance is considered for the first time in a predictive equation.
  • •Predictive equation derived from databases using 3D physical and numerical modeling.
  • •The equation was successfully tested on the 2018 Anak Krakatau tsunami event.
  • •The developed equation using three-dimensional data exhibits a 91 % fitting quality.

Abstract

Landslide tsunamis, responsible for thousands of deaths and significant damage in recent years, necessitate the allocation of sufficient time and resources for studying these extreme natural hazards. This study offers a step change in the field by conducting a large number of three-dimensional numerical experiments, validated by physical tests, to develop a predictive equation for the maximum initial amplitude of tsunamis generated by subaerial landslides. We first conducted a few 3D physical experiments in a wave basin which were then applied for the validation of a 3D numerical model based on the Flow3D-HYDRO package. Consequently, we delivered 100 simulations using the validated model by varying parameters such as landslide volume, water depth, slope angle and travel distance. This large database was subsequently employed to develop a predictive equation for the maximum initial tsunami amplitude. For the first time, we considered travel distance as an independent parameter for developing the predictive equation, which can significantly improve the predication accuracy. The predictive equation was tested for the case of the 2018 Anak Krakatau subaerial landslide tsunami and produced satisfactory results.

Keywords

Tsunami, Subaerial landslide, Physical modelling, Numerical simulation, FLOW-3D HYDRO

1. Introduction and literature review

The Anak Krakatau landslide tsunami on 22nd December 2018 was a stark reminder of the dangers posed by subaerial landslide tsunamis (Ren et al., 2020Mulia et al. 2020a; Borrero et al., 2020Heidarzadeh et al., 2020Grilli et al., 2021). The collapse of the volcano’s southwest side into the ocean triggered a tsunami that struck the Sunda Strait, leading to approximately 450 fatalities (Syamsidik et al., 2020Mulia et al., 2020b) (Fig. 1). As shown in Fig. 1, landslide tsunamis (both submarine and subaerial) have been responsible for thousands of deaths and significant damage to coastal communities worldwide. These incidents underscored the critical need for advanced research into landslide-generated waves to aid in hazard prediction and mitigation. This is further emphasized by recent events such as the 28th of November 2020 landslide tsunami in the southern coast mountains of British Columbia (Canada), where an 18 million m3 rockslide generated a massive tsunami, with over 100 m wave run-up, causing significant environmental and infrastructural damage (Geertsema et al., 2022).

Fig 1

Physical modelling and numerical simulation are crucial tools in the study of landslide-induced waves due to their ability to replicate and analyse the complex dynamics of landslide events (Kim et al., 2020). In two-dimensional (2D) modelling, the discrepancy between dimensions can lead to an artificial overestimation of wave amplification (e.g., Heller and Spinneken, 2015). This limitation is overcome with 3D modelling, which enables the scaled-down representation of landslide-generated waves while avoiding the simplifications inherent in 2D approaches (Erosi et al., 2019). Another advantage of 3D modelling in studying landslide-generated waves is its ability to accurately depict the complex dynamics of wave propagation, including lateral and radial spreading from the slide impact zone, a feature unattainable with 2D models (Heller and Spinneken, 2015).

Physical experiments in tsunami research, as presented by authors such as Romano et al. (2020), McFall and Fritz (2016), and Heller and Spinneken (2015), have supported 3D modelling works through validation and calibration of the numerical models to capture the complexities of wave generation and propagation. Numerical modelling has increasingly complemented experimental approach in tsunami research due to the latter’s time and resource-intensive nature, particularly for 3D models (Li et al., 2019; Kim et al., 2021). Various numerical approaches have been employed, from Eulerian and Lagrangian frameworks to depth-averaged and Navier–Stokes models, enhancing our understanding of tsunami dynamics (Si et al., 2018Grilli et al., 2019Heidarzadeh et al., 20172020Iorio et al., 2021Zhang et al., 2021Kirby et al., 2022Wang et al., 20212022Hu et al., 2022). The sophisticated numerical techniques, including the Particle Finite Element Method and the Immersed Boundary Method, have also shown promising results in modelling highly dynamic landslide scenarios (Mulligan et al., 2020Chen et al., 2020). Among these methods and techniques, FLOW-3D HYDRO stands out in simulating landslide-generated tsunami waves due to its sophisticated technical features such as offering Tru Volume of Fluid (VOF) method for precise free surface tracking (e.g., Sabeti and Heidarzadeh 2022a). TruVOF distinguishes itself through a split Lagrangian approach, adeptly reducing cumulative volume errors in wave simulations by dynamically updating cell volume fractions and areas with each time step. Its intelligent adaptation of time step size ensures precise capture of evolving free surfaces, offering unparalleled accuracy in modelling complex fluid interfaces and behaviour (Flow Science, 2023).

Predictive equations play a crucial role in assessing the potential hazards associated with landslide-generated tsunami waves due to their ability to provide risk assessment and warnings. These equations can offer swift and reasonable evaluations of potential tsunami impacts in the absence of detailed numerical simulations, which can be time-consuming and expensive to produce. Among multiple factors and parameters within a landslide tsunami generation, the initial maximum wave amplitude (Fig. 1) stands out due to its critical role. While it is most likely that the initial wave generated by a landslide will have the highest amplitude, it is crucial to clarify that the term “initial maximum wave amplitude” refers to the highest amplitude within the first set of impulse waves. This parameter is essential in determining the tsunami’s impact severity, with higher amplitudes signalling a greater destructive potential (Sabeti and Heidarzadeh 2022a). Additionally, it plays a significant role in tsunami modelling, aiding in the prediction of wave propagation and the assessment of potential impacts.

In this study, we initially validate the FLOW-3D HYDRO model through a series of physical experiments conducted in a 3D wave tank at University of Bath (UK). Upon confirmation of the model’s accuracy, we use it to systematically vary parameters namely landslide volume, water depth, slope angle, and travel distance, creating an extensive database. Alongside this, we perform a sensitivity analysis on these variables to discern their impacts on the initial maximum wave amplitude. The generated database was consequently applied to derive a non-dimensional predictive equation aimed at estimating the initial maximum wave amplitude in real-world landslide tsunami events.

Two innovations of this study are: (i) The predictive equation of this study is based on a large number of 3D experiments whereas most of the previous equations were based on 2D results, and (ii) For the first time, the travel distance is included in the predictive equation as an independent parameter. To evaluate the performance of our predictive equation, we applied it to a previous real-world subaerial landslide tsunami, i.e., the Anak Krakatau 2018 event. Furthermore, we compare the performance of our predictive equation with other existing equations.

2. Data and methods

The methodology applied in this research is a combination of physical and numerical modelling. Limited physical modelling was performed in a 3D wave basin at the University of Bath (UK) to provide data for calibration and validation of the numerical model. After calibration and validation, the numerical model was employed to model a large number of landslide tsunami scenarios which allowed us to develop a database for deriving a predictive equation.

2.1. Physical experiments

To validate our numerical model, we conducted a series of physical experiments including two sets in a 3D wave basin at University of Bath, measuring 2.50 m in length (WL), 2.60 m in width (WW), and 0.60 m in height (WH) (Fig. 2a). Conducting two distinct sets of experiments (Table 1), each with different setups (travel distance, location, and water depth), provided a robust framework for validation of the numerical model. For wave measurement, we employed a twin wire wave gauge from HR Wallingford (https://equipit.hrwallingford.com). In these experiments, we used a concrete prism solid block, the dimensions of which are outlined in Table 2. In our experiments, we employed a concrete prism solid block with a density of 2600 kg/m3, chosen for its similarity to the natural density of landslides, akin to those observed with the 2018 Anak Krakatau tsunami, where the landslide composition is predominantly solid rather than granular. The block’s form has also been endorsed in prior studies (Watts, 1998Najafi-Jilani and Ataie-Ashtiani, 2008) as a suitable surrogate for modelling landslide-induced waves. A key aspect of our methodology was addressing scale effects, following the guidelines proposed by Heller et al. (2008) as it is described in Table 1. To enhance the reliability and accuracy of our experimental data, we conducted each physical experiment three times which revealed all three experimental waveforms were identical. This repetition was aimed at minimizing potential errors and inconsistencies in laboratory measurements.

Fig 2

Table 1. The locations and other information of the laboratory setups for making landslide-generated waves in the physical wave basin. This table details the specific parameters for each setup, including slope range (α), slide volume (V), kinematic viscosity (ν), water depth (h), travel distance (D), surface tension coefficient of water (σ), Reynolds number (R), Weber number (W), and the precise coordinates of the wave gauges (WG).

Labα(°)V (m³)h (m)D (m)WG’s Location(ν) (m²/s)(σ) (N/m)Acceptable range for avoiding scale effects*Observed values of W and R ⁎⁎
Lab 1452.60 × 10−30.2470.070X1=1.090 m1.01 × 10−60.073R > 3.0 × 105R1 = 3.80 × 105
Y1=1.210 m
W1 = 8.19 × 105
Z1=0.050mW >5.0 × 103
Lab 2452.60 × 10−30.2460.045X2=1.030 m1.01 × 10−60.073R2 = 3.78 × 105
Y2=1.210 mW2 = 8.13 × 105
Z2=0.050 m

The acceptable ranges for avoiding scale effects are based on the study by Heller et al. (2008).⁎⁎

The Reynolds number (R) is given by g0.5h1.5/ν, with ν denoting the kinematic viscosity. The Weber number (W) is W = ρgh2/σ, where σ represents surface tension coefficient and ρ = 1000kg/m3 is the density of water. In our experiments, conducted at a water temperature of approximately 20 °C, the kinematic viscosity (ν) and the surface tension coefficient of water (σ) are 1.01 × 10−6 m²/s and 0.073 N/m, respectively (Kestin et al., 1978).

Table 2. Specifications of the solid block used in physical experiments for generating subaerial landslides in the laboratory.

Solid-block attributesProperty metricsGeometric shape
Slide width (bs)0.26 mImage, table 2
Slide length (ls)0.20 m
Slide thickness (s)0.10 m
Slide volume (V)2.60 × 10−3 m3
Specific gravity, (γs)2.60
Slide weight (ms)6.86 kg

2.2. Numerical simulations applying FLOW-3D hydro

The detailed theoretical framework encompassing the governing equations, the computational methodologies employed, and the specific techniques used for tracking the water surface in these simulations are thoroughly detailed in the study by Sabeti et al. (2024). Here, we briefly explain some of the numerical details. We defined a uniform mesh for our flow domain, carefully crafted with a fine spatial resolution of 0.005 m (i.e., grid size). The dimensions of the numerical model directly matched those of our wave basin used in the physical experiment, being 2.60 m wide, 0.60 m deep, and 2.50 m long (Fig. 2). This design ensures comprehensive coverage of the study area. The output intervals of the numerical model are set at 0.02 s. This timing is consistent with the sampling rates of wave gauges used in laboratory settings. The friction coefficient in the FLOW-3D HYDRO is designated as 0.45. This value corresponds to the Coulombic friction measurements obtained in the laboratory, ensuring that the simulation accurately reflects real-world physical interactions.

In order to simulate the landslide motion, we applied coupled motion objects in FLOW-3D-HYDRO where the dynamics are predominantly driven by gravity and surface friction. This methodology stands in contrast to other models that necessitate explicit inputs of force and torque. This approach ensures that the simulation more accurately reflects the natural movement of landslides, which is heavily reliant on gravitational force and the interaction between sliding surfaces. The stability of the numerical simulations is governed by the Courant Number criterion (Courant et al., 1928), which dictates the maximum time step (Δt) for a given mesh size (Δx) and flow speed (U). According to Courant et al. (1928), this number is required to stay below one to ensure stability of numerical simulations. In our simulations, the Courant number is always maintained below one.

In alignment with the parameters of physical experiments, we set the fluid within the mesh to water, characterized by a density of 1000 kg/m³ at a temperature of 20 °C. Furthermore, we defined the top, front, and back surfaces of the mesh as symmetry planes. The remaining surfaces are designated as wall types, incorporating no-slip conditions to accurately simulate the interaction between the fluid and the boundaries. In terms of selection of an appropriate turbulence model, we selected the k–ω model that showed a better performance than other turbulence methods (e.g., Renormalization-Group) in a previous study (Sabeti et al., 2024). The simulations are conducted using a PC Intel® Core™ i7-10510U CPU with a frequency of 1.80 GHz, and a 16 GB RAM. On this PC, completion of a 3-s simulation required approximately 12.5 h.

2.3. Validation

The FLOW-3D HYDRO numerical model was validated using the two physical experiments (Fig. 3) outlined in Table 1. The level of agreement between observations (Oi) and simulations (Si) is examined using the following equation:(1)�=|��−����|×100where ε represents the mismatch error, Oi denotes the observed laboratory values, and Si represents the simulated values from the FLOW-3D HYDRO model. The results of this validation process revealed that our model could replicate the waves generated in the physical experiments with a reasonable degree of mismatch (ε): 14 % for Lab 1 and 8 % for Lab 2 experiments, respectively (Fig. 3). These values indicate that while the model is not perfect, it provides a sufficiently close approximation of the real-world phenomena.

Fig 3

In terms of mesh efficiency, we varied the mesh size to study sensitivity of the numerical results to mesh size. First, by halving the mesh size and then by doubling it, we repeated the modelling by keeping other parameters unchanged. This analysis guided that a mesh size of ∆x = 0.005 m is the most effective for the setup of this study. The total number of computational cells applying mesh size of 0.005 m is 9.269 × 106.

2.4. The dataset

The validated numerical model was employed to conduct 100 simulations, incorporating variations in four key landslide parameters namely water depth, slope angle, slide volume, and travel distance. This methodical approach was essential for a thorough sensitivity analysis of these variables, and for the creation of a detailed database to develop a predictive equation for maximum initial tsunami amplitude. Within the model, 15 distinct slide volumes were established, ranging from 0.10 × 10−3 m3 to 6.25 × 10−3 m3 (Table 3). The slope angle varied between 35° and 55°, and water depth ranged from 0.24 m to 0.27 m. The travel distance of the landslides was varied, spanning from 0.04 m to 0.07 m. Detailed configurations of each simulation, along with the maximum initial wave amplitudes and dominant wave periods are provided in Table 4.

Table 3. Geometrical information of the 15 solid blocks used in numerical modelling for generating landslide tsunamis. Parameters are: ls, slide length; bs, slide width; s, slide thickness; γs, specific gravity; and V, slide volume.

Solid blockls (m)bs (m)s (m)V (m3)γs
Block-10.3100.2600.1556.25 × 10−32.60
Block-20.3000.2600.1505.85 × 10−32.60
Block-30.2800.2600.1405.10 × 10−32.60
Block-40.2600.2600.1304.39 × 10−32.60
Block-50.2400.2600.1203.74 × 10−32.60
Block-60.2200.2600.1103.15 × 10−32.60
Block-70.2000.2600.1002.60 × 10−32.60
Block-80.1800.2600.0902.11 × 10−32.60
Block-90.1600.2600.0801.66 × 10−32.60
Block-100.1400.2600.0701.27 × 10−32.60
Block-110.1200.2600.0600.93 × 10−32.60
Block-120.1000.2600.0500.65 × 10−32.60
Block-130.0800.2600.0400.41 × 10−32.60
Block-140.0600.2600.0300.23 × 10−32.60
Block-150.0400.2600.0200.10 × 10−32.60

Table 4. The numerical simulation for the 100 tests performed in this study for subaerial solid-block landslide-generated waves. Parameters are aM, maximum wave amplitude; α, slope angle; h, water depth; D, travel distance; and T, dominant wave period. The location of the wave gauge is X=1.030 m, Y=1.210 m, and Z=0.050 m. The properties of various solid blocks are presented in Table 3.

Test-Block Noα (°)h (m)D (m)T(s)aM (m)
1Block-7450.2460.0290.5100.0153
2Block-7450.2460.0300.5050.0154
3Block-7450.2460.0310.5050.0156
4Block-7450.2460.0320.5050.0158
5Block-7450.2460.0330.5050.0159
6Block-7450.2460.0340.5050.0160
7Block-7450.2460.0350.5050.0162
8Block-7450.2460.0360.5050.0166
9Block-7450.2460.0370.5050.0167
10Block-7450.2460.0380.5050.0172
11Block-7450.2460.0390.5050.0178
12Block-7450.2460.0400.5050.0179
13Block-7450.2460.0410.5050.0181
14Block-7450.2460.0420.5050.0183
15Block-7450.2460.0430.5050.0190
16Block-7450.2460.0440.5050.0197
17Block-7450.2460.0450.5050.0199
18Block-7450.2460.0460.5050.0201
19Block-7450.2460.0470.5050.0191
20Block-7450.2460.0480.5050.0217
21Block-7450.2460.0490.5050.0220
22Block-7450.2460.0500.5050.0226
23Block-7450.2460.0510.5050.0236
24Block-7450.2460.0520.5050.0239
25Block-7450.2460.0530.5100.0240
26Block-7450.2460.0540.5050.0241
27Block-7450.2460.0550.5050.0246
28Block-7450.2460.0560.5050.0247
29Block-7450.2460.0570.5050.0248
30Block-7450.2460.0580.5050.0249
31Block-7450.2460.0590.5050.0251
32Block-7450.2460.0600.5050.0257
33Block-1450.2460.0450.5050.0319
34Block-2450.2460.0450.5050.0294
35Block-3450.2460.0450.5050.0282
36Block-4450.2460.0450.5050.0262
37Block-5450.2460.0450.5050.0243
38Block-6450.2460.0450.5050.0223
39Block-7450.2460.0450.5050.0196
40Block-8450.2460.0450.5050.0197
41Block-9450.2460.0450.5050.0198
42Block-10450.2460.0450.5050.0184
43Block-11450.2460.0450.5050.0173
44Block-12450.2460.0450.5050.0165
45Block-13450.2460.0450.4040.0153
46Block-14450.2460.0450.4040.0124
47Block-15450.2460.0450.5050.0066
48Block-7450.2020.0450.4040.0220
49Block-7450.2040.0450.4040.0219
50Block-7450.2060.0450.4040.0218
51Block-7450.2080.0450.4040.0217
52Block-7450.2100.0450.4040.0216
53Block-7450.2120.0450.4040.0215
54Block-7450.2140.0450.5050.0214
55Block-7450.2160.0450.5050.0214
56Block-7450.2180.0450.5050.0213
57Block-7450.2200.0450.5050.0212
58Block-7450.2220.0450.5050.0211
59Block-7450.2240.0450.5050.0208
60Block-7450.2260.0450.5050.0203
61Block-7450.2280.0450.5050.0202
62Block-7450.2300.0450.5050.0201
63Block-7450.2320.0450.5050.0201
64Block-7450.2340.0450.5050.0200
65Block-7450.2360.0450.5050.0199
66Block-7450.2380.0450.4040.0196
67Block-7450.2400.0450.4040.0194
68Block-7450.2420.0450.4040.0193
69Block-7450.2440.0450.4040.0192
70Block-7450.2460.0450.5050.0190
71Block-7450.2480.0450.5050.0189
72Block-7450.2500.0450.5050.0187
73Block-7450.2520.0450.5050.0187
74Block-7450.2540.0450.5050.0186
75Block-7450.2560.0450.5050.0184
76Block-7450.2580.0450.5050.0182
77Block-7450.2590.0450.5050.0183
78Block-7450.2600.0450.5050.0191
79Block-7450.2610.0450.5050.0192
80Block-7450.2620.0450.5050.0194
81Block-7450.2630.0450.5050.0195
82Block-7450.2640.0450.5050.0195
83Block-7450.2650.0450.5050.0197
84Block-7450.2660.0450.5050.0197
85Block-7450.2670.0450.5050.0198
86Block-7450.2700.0450.5050.0199
87Block-7300.2460.0450.5050.0101
88Block-7350.2460.0450.5050.0107
89Block-7360.2460.0450.5050.0111
90Block-7370.2460.0450.5050.0116
91Block-7380.2460.0450.5050.0117
92Block-7390.2460.0450.5050.0119
93Block-7400.2460.0450.5050.0121
94Block-7410.2460.0450.5050.0127
95Block-7420.2460.0450.4040.0154
96Block-7430.2460.0450.4040.0157
97Block-7440.2460.0450.4040.0162
98Block-7450.2460.0450.5050.0197
99Block-7500.2460.0450.5050.0221
100Block-7550.2460.0450.5050.0233

In all these 100 simulations, the wave gauge was consistently positioned at coordinates X=1.09 m, Y=1.21 m, and Z=0.05 m. The dominant wave period for each simulation was determined using the Fast Fourier Transform (FFT) function in MATLAB (MathWorks, 2023). Furthermore, the classification of wave types was carried out using a wave categorization graph according to Sorensen (2010), as shown in Fig. 4a. The results indicate that the majority of the simulated waves are on the border between intermediate and deep-water waves, and they are categorized as Stokes waves (Fig. 4a). Four sample waveforms from our 100 numerical experiments are provided in Fig. 4b.

Fig 4

The dataset in Table 4 was used to derive a new predictive equation that incorporates travel distance for the first time to estimate the initial maximum tsunami amplitude. In developing this equation, a genetic algorithm optimization technique was implemented using MATLAB (MathWorks 2023). This advanced approach entailed the use of genetic algorithms (GAs), an evolutionary algorithm type inspired by natural selection processes (MathWorks, 2023). This technique is iterative, involving selection, crossover, and mutation processes to evolve solutions over several generations. The goal was to identify the optimal coefficients and powers for each landslide parameter in the predictive equation, ensuring a robust and reliable model for estimating maximum wave amplitudes. Genetic Algorithms excel at optimizing complex models by navigating through extensive combinations of coefficients and exponents. GAs effectively identify highly suitable solutions for the non-linear and complex relationships between inputs (e.g., slide volume, slope angle, travel distance, water depth) and the output (i.e., maximum initial wave amplitude, aM). MATLAB’s computational environment enhances this process, providing robust tools for GA to adapt and evolve solutions iteratively, ensuring the precision of the predictive model (Onnen et al., 1997). This approach leverages MATLAB’s capabilities to fine-tune parameters dynamically, achieving an optimal equation that accurately estimates aM. It is important to highlight that the nondimensionalized version of this dataset is employed to develop a predictive equation which enables the equation to reproduce the maximum initial wave amplitude (aM) for various subaerial landslide cases, independent of their dimensional differences (e.g., Heler and Hager 2014Heller and Spinneken 2015Sabeti and Heidarzadeh 2022b). For this nondimensionalization, we employed the water depth (h) to nondimensionalize the slide volume (V/h3) and travel distance (D/h). The slide thickness (s) was applied to nondimensionalize the water depth (h/s).

2.5. Landslide velocity

In discussing the critical role of landslide velocity for simulating landslide-generated waves, we focus on the mechanisms of landslide motion and the techniques used to record landslide velocity in our simulations (Fig. 5). Also, we examine how these methods were applied in two distinct scenarios: Lab 1 and Lab 2 (see Table 1 for their details). Regarding the process of landslide movement, a slide starts from a stationary state, gaining momentum under the influence of gravity and this acceleration continues until the landslide collides with water, leading to a significant reduction in its speed before eventually coming to a stop (Fig. 5) (e.g., Panizzo et al. 2005).

Fig 5

To measure the landslide’s velocity in our simulations, we attached a probe at the centre of the slide, which supplied a time series of the velocity data. The slide’s velocity (vs) peaks at the moment it enters the water (Fig. 5), a point referred to as the impact time (tImp). Following this initial impact, the slides continue their underwater movement, eventually coming to a complete halt (tStop). Given the results in Fig. 5, it can be seen that Lab 1, with its longer travel distance (0.070 m), exhibits a higher peak velocity of 1.89 m/s. This increase in velocity is attributed to the extended travel distance allowing more time for the slide to accelerate under gravity. Whereas Lab 2, featuring a shorter travel distance (0.045 m), records a lower peak velocity of 1.78 m/s. This difference underscores how travel distance significantly influences the dynamics of landslide motion. After reaching the peak, both profiles show a sharp decrease in velocity, marking the transition to submarine motion until the slides come to a complete stop (tStop). There are noticeable differences observable in Fig. 5 between the Lab-1 and Lab-2 simulations, including the peaks at 0.3 s . These variations might stem from the placement of the wave gauge, which differs slightly in each scenario, as well as the water depth’s minor discrepancies and, the travel distance.

2.6. Effect of air entrainment

In this section we examine whether it is required to consider air entrainment for our modelling or not as the FLOW-3D HYDRO package is capable of modelling air entrainment. The process of air entrainment in water during a landslide tsunami and its subsequent transport involve two key components: the quantification of air entrainment at the water surface, and the simulation of the air’s transport within the fluid (Hirt, 2003). FLOW-3D HYDRO employs the air entrainment model to compute the volume of air entrained at the water’s surface utilizing three approaches: a constant density model, a variable density model accounting for bulking, and a buoyancy model that adds the Drift-FLUX mechanism to variable density conditions (Flow Science, 2023). The calculation of the entrainment rate is based on the following equation:(2)�������=������[2(��−�����−2�/���)]1/2where parameters are: Vair, volume of air; Cair, entrainment rate coefficient; As, surface area of fluid; ρ, fluid density; k, turbulent kinetic energy; gn, gravity normal to surface; Lt, turbulent length scale; and σ, surface tension coefficient. The value of k is directly computed from the Reynolds-averaged Navier-Stokes (RANS) (kw) calculations in our model.

In this study, we selected the variable density + Drift-FLUX model, which effectively captures the dynamics of phase separation and automatically activates the constant density and variable density models. This method simplifies the air-water mixture, treating it as a single, homogeneous fluid within each computational cell. For the phase volume fractions f1and f2​, the velocities are expressed in terms of the mixture and relative velocities, denoted as u and ur, respectively, as follows:(3)��1��+�.(�1�)=��1��+�.(�1�)−�.(�1�2��)=0(4)��2��+�.(�2�)=��2��+�.(�2�)−�.(�1�2��)=0

The outcomes from this simulation are displayed in Fig. 6, which indicates that the influence of air entrainment on the generated wave amplitude is approximately 2 %. A value of 0.02 for the entrained air volume fraction means that, in the simulated fluid, approximately 2 % of the volume is composed of entrained air. In other words, for every unit volume of the fluid-air mixture at that location, 2 % is air and the remaining 98 % is water. The configuration of Test-17 (Table 4) was employed for this simulation. While the effect of air entrainment is anticipated to be more significant in models of granular landslide-generated waves (Fritz, 2002), in our simulations we opted not to incorporate this module due to its negligible impact on the results.

Fig 6

3. Results

In this section, we begin by presenting a sequence of our 3D simulations capturing different time steps to illustrate the generation process of landslide-generated waves. Subsequently, we derive a new predictive equation to estimate the maximum initial wave amplitude of landslide-generated waves and assess its performance.

3.1. Wave generation and propagation

To demonstrate the wave generation process in our simulation, we reference Test-17 from Table 4, where we employed Block-7 (Tables 34). In this configuration, the slope angle was set to 45°, with a water depth of 0.246 m and a travel distance at 0.045 m (Fig. 7). At 0.220 s, the initial impact of the moving slide on the water is depicted, marking the onset of the wave generation process (Fig. 7a). Disturbances are localized to the immediate area of impact, with the rest of the water surface remaining undisturbed. At this time, a maximum water particle velocity of 1.0 m/s – 1.2 m/s is seen around the impact zone (Fig. 7d). Moving to 0.320 s, the development of the wave becomes apparent as energy transfer from the landslide to the water creates outwardly radiating waves with maximum water particle velocity of up to around 1.6 m/s – 1.8 m/s (Fig. 7b, e). By the time 0.670 s, the wave has fully developed and is propagating away from the impact point exhibiting maximum water particle velocity of up to 2.0 m/s – 2.1 m/s. Concentric wave fronts are visible, moving outwards in all directions, with a colour gradient signifying the highest wave amplitude near the point of landslide entry, diminishing with distance (Fig. 7c, f).

Fig 7

3.2. Influence of landslide parameters on tsunami amplitude

In this section, we investigate the effects of various landslide parameters namely slide volume (V), water depth (h), slipe angle (α) and travel distance (D) on the maximum initial wave amplitude (aM). Fig. 8 presents the outcome of these analyses. According to Fig. 8, the slide volume, slope angle, and travel distance exhibit a direct relationship with the wave amplitude, meaning that as these parameters increase, so does the amplitude. Conversely, water depth is inversely related to the maximum initial wave amplitude, suggesting that the deeper the water depth, the smaller the maximum wave amplitude will be (Fig. 8b).

Fig 8

Fig. 8a highlights the pronounced impact of slide volume on the aM, demonstrating a direct correlation between the two variables. For instance, in the range of slide volumes we modelled (Fig. 8a), The smallest slide volume tested, measuring 0.10 × 10−3 m3, generated a low initial wave amplitude (aM= 0.0066 m) (Table 4). In contrast, the largest volume tested, 6.25 × 10−3 m3, resulted in a significantly higher initial wave amplitude (aM= 0.0319 m) (Table 4). The extremities of these results emphasize the slide volume’s paramount impact on wave amplitude, further elucidated by their positions as the smallest and largest aM values across all conducted tests (Table 4). This is corroborated by findings from the literature (e.g., Murty, 2003), which align with the observed trend in our simulations.

The slope angle’s influence on aM was smooth. A steady increase of wave amplitude was observed as the slope angle increased (Fig. 8c). In examining travel distance, an anomaly was identified. At a travel distance of 0.047 m, there was an unexpected dip in aM, which deviates from the general increasing trend associated with longer travel distances. This singular instance could potentially be attributed to a numerical error. Beyond this point, the expected pattern of increasing aM with longer travel distances resumes, suggesting that the anomaly at 0.047 m is an outlier in an otherwise consistent trend, and thus this single data point was overlooked while deriving the predictive equation. Regarding the inverse relationship between water depth and wave amplitude, our result (Fig. 8b) is consistent with previous reports by Fritz et al. (2003), (2004), and Watts et al. (2005).

The insights from Fig. 8 informed the architecture of the predictive equation in the next Section, with slide volume, travel distance, and slope angle being multiplicatively linked to wave amplitude underscoring their direct correlations with wave amplitude. Conversely, water depth is incorporated as a divisor, representing its inverse relationship with wave amplitude. This structure encapsulates the dynamics between the landslide parameters and their influence on the maximum initial wave amplitude as discussed in more detail in the next Section.

3.3. Predictive equation

Building on our sensitivity analysis of landslide parameters, as detailed in Section 3.2, and utilizing our nondimensional dataset, we have derived a new predictive equation as follows:(5)��/ℎ=0.015(tan�)0.10(�ℎ3)0.90(�ℎ)0.10(ℎ�)−0.11where, V is sliding volume, h is water depth, α is slope angle, and s is landslide thickness. It is important to note that this equation is valid only for subaerial solid-block landslide tsunamis as all our experiments were for this type of waves. The performance of this equation in predicting simulation data is demonstrated by the satisfactory alignment of data points around a 45° line, indicating its accuracy and reliability with regard to the experimental dataset (Fig. 9). The quality of fit between the dataset and Eq. (5) is 91 % indicating that Eq. (5) represents the dataset very well. Table 5 presents Eq. (5) alongside four other similar equations previously published. Two significant distinctions between our Eq. (5) and these others are: (i) Eq. (5) is derived from 3D experiments, whereas the other four equations are based on 2D experiments. (ii) Unlike the other equations, our Eq. (5) incorporates travel distance as an independent parameter.

Fig 9

Table 5. Performance comparison among our newly-developed equation and existing equations for estimating the maximum initial amplitude (aM) of the 2018 Anak Krakatau subaerial landslide tsunami. Parameters: aM, initial maximum wave amplitude; h, water depth; vs, landslide velocity; V, slide volume; bs, slide width; ls, slide length; s, slide thickness; α, slope angle; and ����, volume of the final immersed landslide. We considered ����= V as the slide volume.

EventPredictive equationsAuthor (year)Observed aM (m) ⁎⁎Calculated aM (m)Error, ε (%) ⁎⁎⁎⁎
2018 Anak Krakatau tsunami (Subaerial landslide) *��/ℎ=1.32���ℎNoda (1970)1341340
��/ℎ=0.667(0.5(���ℎ)2)0.334(���)0.754(���)0.506(�ℎ)1.631Bolin et al. (2014) ⁎⁎⁎13459424334
��/ℎ=0.25(������ℎ2)0.8Robbe-Saule et al. (2021)1343177
��/ℎ=0.4545(tan�)0.062(�ℎ3)0.296(ℎ�)−0.235Sabeti and Heidarzadeh (2022b)1341266
��/ℎ=0.015(tan�)0.10(�ℎ3)0.911(�ℎ)0.10(ℎ�)−0.11This study1341302.9

Geometrical and kinematic parameters of the 2018 Anak Krakatau subaerial landslide based on Heidarzadeh et al. (2020)Grilli et al. (2019) and Grilli et al. (2021)V=2.11 × 107 m3h= 50 m; s= 114 m; α= 45°; ls=1250 m; bs= 2700 m; vs=44.9 m/s; D= 2500 m; aM= 100 m −150 m.⁎⁎

aM= An average value of aM = 134 m is considered in this study.⁎⁎⁎

The equation of Bolin et al. (2014) is based on the reformatted one reported by Lindstrøm (2016).⁎⁎⁎⁎

Error is calculated using Eq. (1), where the calculated aM is assumed as the simulated value.

Additionally, we evaluated the performance of this equation using the real-world data from the 2018 Anak Krakatau subaerial landslide tsunami. Based on previous studies (Heidarzadeh et al., 2020Grilli et al., 20192021), we were able to provide a list of parameters for the subaerial landslide and associated tsunami for the 2018 Anak Krakatau event (see footnote of Table 5). We note that the data of the 2018 Anak Krakatau event was not used while deriving Eq. (5). The results indicate that Eq. (5) predicts the initial amplitude of the 2018 Anak Krakatau tsunami as being 130 m indicating an error of 2.9 % compared to the reported average amplitude of 134 m for this event. This performance indicates an improvement compared to the previous equation reported by Sabeti and Heidarzadeh (2022a) (Table 5). In contrast, the equations from Robbe-Saule et al. (2021) and Bolin et al. (2014) demonstrate higher discrepancies of 4200 % and 77 %, respectively (Table 5). Although Noda’s (1970) equation reproduces the tsunami amplitude of 134 m accurately (Table 5), it is crucial to consider its limitations, notably not accounting for parameters such as slope angle and travel distance.

It is essential to recognize that both travel distance and slope angle significantly affect wave amplitude. In our model, captured in Eq. (5), we integrate the slope angle (α) through the tangent function, i.e., tan α. This choice diverges from traditional physical interpretations that often employ the cosine or sine function (e.g., Heller and Hager, 2014Watts et al., 2003). We opted for the tangent function because it more effectively reflects the direct impact of slope steepness on wave generation, yielding superior estimations compared to conventional methods.

The significance of this study lies in its application of both physical and numerical 3D experiments and the derivation of a predictive equation based on 3D results. Prior research, e.g. Heller et al. (2016), has reported notable discrepancies between 2D and 3D wave amplitudes, highlighting the important role of 3D experiments. It is worth noting that the suitability of applying an equation derived from either 2D or 3D data depends on the specific geometry and characteristics inherent in the problem being addressed. For instance, in the case of a long, narrow dam reservoir, an equation derived from 2D data would likely be more suitable. In such contexts, the primary dynamics of interest such as flow patterns and potential wave propagation are predominantly two-dimensional, occurring along the length and depth of the reservoir. This simplification to 2D for narrow dam reservoirs allows for more accurate modelling of these dynamics.

This study specifically investigates waves initiated by landslides, focusing on those characterized as solid blocks instead of granular flows, with slope angles confined to a range of 25° to 60°. We acknowledge the additional complexities encountered in real-world scenarios, such as dynamic density and velocity of landslides, which could affect the estimations. The developed equation in this study is specifically designed to predict the maximum initial amplitude of tsunamis for the aforementioned specified ranges and types of landslides.

4. Conclusions

Both physical and numerical experiments were undertaken in a 3D wave basin to study solid-block landslide-generated waves and to formulate a predictive equation for their maximum initial wave amplitude. At the beginning, two physical experiments were performed to validate and calibrate a 3D numerical model, which was subsequently utilized to generate 100 experiments by varying different landslide parameters. The generated database was then used to derive a predictive equation for the maximum initial wave amplitude of landslide tsunamis. The main features and outcomes are:

  • •The predictive equation of this study is exclusively derived from 3D data and exhibits a fitting quality of 91 % when applied to the database.
  • •For the first time, landslide travel distance was considered in the predictive equation. This inclusion provides more accuracy and flexibility for applying the equation.
  • •To further evaluate the performance of the predictive equation, it was applied to a real-world subaerial landslide tsunami (i.e., the 2018 Anak Krakatau event) and delivered satisfactory performance.

CRediT authorship contribution statement

Ramtin Sabeti: Conceptualization, Methodology, Validation, Software, Visualization, Writing – review & editing. Mohammad Heidarzadeh: Methodology, Data curation, Software, Writing – review & editing.

Declaration of competing interest

The authors declare that they have no known competing financial interests or personal relationships that could have appeared to influence the work reported in this paper.

Funding

RS is supported by the Leverhulme Trust Grant No. RPG-2022-306. MH is funded by open funding of State Key Lab of Hydraulics and Mountain River Engineering, Sichuan University, grant number SKHL2101. We acknowledge University of Bath Institutional Open Access Fund. MH is also funded by the Great Britain Sasakawa Foundation grant no. 6217 (awarded in 2023).

Acknowledgements

Authors are sincerely grateful to the laboratory technician team, particularly Mr William Bazeley, at the Faculty of Engineering, University of Bath for their support during the laboratory physical modelling of this research. We appreciate the valuable insights provided by Mr. Brian Fox (Senior CFD Engineer at Flow Science, Inc.) regarding air entrainment modelling in FLOW-3D HYDRO. We acknowledge University of Bath Institutional Open Access Fund.

Data availability

  • All data used in this study are given in the body of the article.

References

Figure 3 – Free surface views. Bottom left: k-ε RNG model. Bottom right: LES.

Physical Modeling and CFD Comparison: Case Study of a HydroCombined Power Station in Spillway Mode

물리적 모델링 및 CFD 비교: 방수로 모드의 HydroCombined 발전소 사례 연구

Gonzalo Duró, Mariano De Dios, Alfredo López, Sergio O. Liscia

ABSTRACT

This study presents comparisons between the results of a commercial CFD code and physical model measurements. The case study is a hydro-combined power station operating in spillway mode for a given scenario. Two turbulence models and two scales are implemented to identify the capabilities and limitations of each approach and to determine the selection criteria for CFD modeling for this kind of structure. The main flow characteristics are considered for analysis, but the focus is on a fluctuating frequency phenomenon for accurate quantitative comparisons. Acceptable representations of the general hydraulic functioning are found in all approaches, according to physical modeling. The k-ε RNG, and LES models give good representation of the discharge flow, mean water depths, and mean pressures for engineering purposes. The k-ε RNG is not able to characterize fluctuating phenomena at a model scale but does at a prototype scale. The LES is capable of identifying the dominant frequency at both prototype and model scales. A prototype-scale approach is recommended for the numerical modeling to obtain a better representation of fluctuating pressures for both turbulence models, with the complement of physical modeling for the ultimate design of the hydraulic structures.

본 연구에서는 상용 CFD 코드 결과와 물리적 모델 측정 결과를 비교합니다. 사례 연구는 주어진 시나리오에 대해 배수로 모드에서 작동하는 수력 복합 발전소입니다.

각 접근 방식의 기능과 한계를 식별하고 이러한 종류의 구조에 대한 CFD 모델링의 선택 기준을 결정하기 위해 두 개의 난류 모델과 두 개의 스케일이 구현되었습니다. 주요 흐름 특성을 고려하여 분석하지만 정확한 정량적 비교를 위해 변동하는 주파수 현상에 중점을 둡니다.

일반적인 수리학적 기능에 대한 허용 가능한 표현은 물리적 모델링에 따라 모든 접근 방식에서 발견됩니다. k-ε RNG 및 LES 모델은 엔지니어링 목적을 위한 배출 유량, 평균 수심 및 평균 압력을 잘 표현합니다.

k-ε RNG는 모델 규모에서는 변동 현상을 특성화할 수 없지만 프로토타입 규모에서는 특성을 파악합니다. LES는 프로토타입과 모델 규모 모두에서 주요 주파수를 식별할 수 있습니다.

수력학적 구조의 궁극적인 설계를 위한 물리적 모델링을 보완하여 두 난류 모델에 대한 변동하는 압력을 더 잘 표현하기 위해 수치 모델링에 프로토타입 규모 접근 방식이 권장됩니다.

Figure 1 – Physical scale model (left). Upstream flume and point gauge (right)
Figure 1 – Physical scale model (left). Upstream flume and point gauge (right)
Figure 3 – Free surface views. Bottom left: k-ε RNG model. Bottom right: LES.
Figure 3 – Free surface views. Bottom left: k-ε RNG model. Bottom right: LES.
Figure 4 – Water levels: physical model (maximum values) and CFD results (mean values)
Figure 4 – Water levels: physical model (maximum values) and CFD results (mean values)
Figure 5 – Instantaneous pressures [Pa] and velocities [m/s] at model scale (bay center)
Figure 5 – Instantaneous pressures [Pa] and velocities [m/s] at model scale (bay center)

Keywords

CFD validation, hydro-combined, k-ε RNG, LES, pressure spectrum

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Numerical Investigation of the Local Scour for Tripod Pile Foundation.

Numerical Investigation of the Local Scour for Tripod Pile Foundation.

Hassan, Waqed H.; Fadhe, Zahraa Mohammad; Thiab, Rifqa F.; Mahdi, Karrar

초록

This work investigates numerically a local scour moves in irregular waves around tripods. It is constructed and proven to use the numerical model of the seabed-tripodfluid with an RNG k turbulence model. The present numerical model then examines the flow velocity distribution and scour characteristics. After that, the suggested computational model Flow-3D is a useful tool for analyzing and forecasting the maximum scour development and the flow field in random waves around tripods. The scour values affecting the foundations of the tripod must be studied and calculated, as this phenomenon directly and negatively affects the structure of the structure and its design life. The lower diagonal braces and the main column act as blockages, increasing the flow accelerations underneath them. This increases the number of particles that are moved, which in turn creates strong scouring in the area. The numerical model has a good agreement with the experimental model, with a maximum percentage of error of 10% between the experimental and numerical models. In addition, Based on dimensional analysis parameters, an empirical equation has been devised to forecast scour depth with flow depth, median size ratio, Keulegan-Carpenter (Kc), Froud number flow, and wave velocity that the results obtained in this research at various flow velocities and flow depths demonstrated that the maximum scour depth rate depended on wave height with rising velocities and decreasing particle sizes (d50) and the scour depth attains its steady-current value for Vw < 0.75. As the Froude number rises, the maximum scour depth will be large.

주제어

BUILDING foundationsSURFACE waves (Seismic waves)FLOW velocityRANDOM fieldsDIMENSIONAL analysisFROUDE numberOCEAN waves

키워드

출판물

Mathematical Modelling of Engineering Problems, 2024, Vol 11, Issue 4, p903

ISSN 2369-0739

저자 소속기관

  • 1 Civil Engineering Department, Faculty of Engineering, University of Warith Al-Anbiyaa, Kerbala 56001, Iraq
  • 2 Civil Engineering Department, Faculty of Engineering, University of Kerbala, Kerbala 56001, Iraq
  • 3 Department of Radiological Techniques, College of Health and Medical Techniques, Al-Zahraa University for Women, Karbala 56100, Iraq
  • 4 Soil Physics and Land Management Group, Wageningen University & Research, Wageningen 6708 PB, Netherlands
Figure (17): Stream Lines Indicating Average Flow Speed in the Model with Various Nose shapes, Measured at Mid-Depth and at the Flow Surface Level, at a Flow Rate of 78 Liters per Second.

Conducting experimental and numerical studies to analyze theimpact of the base nose shape on flow hydraulics in PKW weirusing FLOW-3D

FLOW-3D를 사용하여 PKW 둑의 흐름 수력학에 대한 베이스 노즈 모양의 영향을 분석하기 위한 실험 및 수치 연구 수행

Behshad Mardasi 1
Rasoul Ilkhanipour Zeynali 2
Majid Heydari 3

Abstract

Weirs are essential structures used to manage excess water flow from behind dams to downstream areas. Enhancing discharge efficiency often involves extending the effective length of Piano Key Weirs (PKW) in dams or regulating flow within irrigation and drainage networks. This study employed both numerical and laboratory investigations to assess the impact of different base nose shapes installed beneath the outlet keys and varying Input to output key width ratios (Wi/Wo) on discharges ranging from 5 to 80 liters per second. Furthermore, the study aimed to achieve research objectives and compare the performance of Piano Key Weirs with Ogee Weir. For numerical simulation, the optimal number of cells for meshing was determined, and an appropriate turbulence model was selected. The results indicated that the numerical model accurately simulated the laboratory sample with a high degree of precision. Moreover, the numerical model closely approximated PKW for all parameters Q, H, and Cd compared to the laboratory sample. The findings revealed that in laboratory models with a maximum discharge area of 80 liters per second, the weir with Wi/Wo=1.2 and a flow head value of 285 mm exhibited the lowest value, whereas the weir with Wi/Wo=0.71 and a flow head value of 305 mm showed the highest, attributed to the higher discharge in the input-output ratio. Additionally, as the ratio of flow head to weir height H/P increased, the discharge coefficient Cd decreased. Comparing the flow conditions in weirs with different base nose shapes, it was observed that the weir with a spindle nose shape (PKW1.2S) outperformed the PKW with a flat (PKW1.2), semi-cylindrical (PKW1.2CL) and triangular base nose (PKW1.2TR). The results emphasized that models featuring semi-cylindrical and flat noses exhibited notable flow deviation and abrupt disruption upon impact with the nose. However, this effect was significantly reduced in models equipped with triangular and spindle-shaped noses. Also, the coefficient of discharge in PKW1.2S and PKW1.2TR weirs, compared to the PKW1.20 weir, increased by 27% and 20%, respectively.

웨어는 댐 뒤에서 하류 지역으로의 과도한 물 흐름을 관리하는 데 사용되는 필수 구조물입니다. 배출 효율을 높이는 데에는 댐의 피아노 키 위어(PKW) 유효 길이를 연장하거나 관개 및 배수 네트워크 내 흐름을 조절하는 것이 포함됩니다.

이 연구에서는 콘센트 키 아래에 설치된 다양한 베이스 노즈 모양과 초당 5~80리터 범위의 배출에 대한 다양한 입력 대 출력 키 너비 비율(Wi/Wo)의 영향을 평가하기 위해 수치 및 실험실 조사를 모두 사용했습니다. 또한 본 연구에서는 연구 목적을 달성하고 Piano Key Weir와 Ogee Weir의 성능을 비교하는 것을 목표로 했습니다.

수치 시뮬레이션을 위해 메시 생성을 위한 최적의 셀 수를 결정하고 적절한 난류 모델을 선택했습니다. 결과는 수치 모델이 높은 정밀도로 실험실 샘플을 정확하게 시뮬레이션했음을 나타냅니다. 더욱이, 수치 모델은 실험실 샘플과 비교하여 모든 매개변수 Q, H 및 Cd에 대해 PKW에 매우 근접했습니다.

연구 결과, 최대 배출 면적이 초당 80리터인 실험실 모델에서는 Wi/Wo=1.2, 플로우 헤드 값이 285mm인 웨어가 가장 낮은 값을 나타냈고, Wi/Wo=0.71 및 a인 웨어는 가장 낮은 값을 나타냈습니다. 플로우 헤드 값은 305mm로 가장 높은 것으로 나타났는데, 이는 입출력 비율의 높은 토출량에 기인합니다. 또한, 웨어 높이에 대한 유수두 비율 H/P가 증가함에 따라 유출계수 Cd는 감소하였다.

베이스 노즈 모양이 다른 웨어의 흐름 조건을 비교해 보면, 스핀들 노즈 모양(PKW1.2S)의 웨어가 평면(PKW1.2), 반원통형(PKW1.2CL) 및 삼각형 모양의 PKW보다 성능이 우수한 것으로 관찰되었습니다. 베이스 노즈(PKW1.2TR) 결과는 반원통형 및 편평한 노즈를 특징으로 하는 모델이 노즈에 충격을 가할 때 눈에 띄는 흐름 편차와 급격한 중단을 나타냄을 강조했습니다.

그러나 삼각형 및 방추형 노즈를 장착한 모델에서는 이러한 효과가 크게 감소했습니다. 또한 PKW1.20보에 비해 PKW1.2S보와 PKW1.2TR보의 유출계수는 각각 27%, 20% 증가하였다.

Keywords

Piano Key Weir, Base Nose Shape, Flow Hydraulics, Numerical Model, Triangular
Nose Shape, Flat Nose Shape, Semi-Cylindrical Nose Shape, Spindle Nose Shape

Figure (17): Stream Lines Indicating Average Flow Speed in the Model with Various Nose shapes, Measured at Mid-Depth and at the Flow Surface Level, at a Flow Rate of 78 Liters per Second.
Figure (17): Stream Lines Indicating Average Flow Speed in the Model with Various Nose shapes, Measured at Mid-Depth and at the Flow Surface Level, at a Flow Rate of 78 Liters per Second.

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Fig. 3. Free surface and substrate profiles in all Sp and Ls cases at t = 1 s, t = 3 s, and t = 5 s, arranged left to right (note: the colour contours correspond to the horizontal component of the flow velocity (u), expressed in m/s).

Numerical investigation of dam break flow over erodible beds with diverse substrate level variations

다양한 기질 수준 변화를 갖는 침식성 층 위의 댐 파손 흐름에 대한 수치 조사

Alireza Khoshkonesh1, Blaise Nsom2, Saeid Okhravi3*, Fariba Ahmadi Dehrashid4, Payam Heidarian5,
Silvia DiFrancesco6
1 Department of Geography, School of Social Sciences, History, and Philosophy, Birkbeck University of London, London, UK.
2 Université de Bretagne Occidentale. IRDL/UBO UMR CNRS 6027. Rue de Kergoat, 29285 Brest, France.
3 Institute of Hydrology, Slovak Academy of Sciences, Dúbravská cesta 9, 84104, Bratislava, Slovak Republic.
4Department of Water Science and Engineering, Faculty of Agriculture, Bu-Ali Sina University, 65178-38695, Hamedan, Iran.
5 Department of Civil, Environmental, Architectural Engineering and Mathematics, University of Brescia, 25123 Brescia, Italy.
6Niccol`o Cusano University, via Don C. Gnocchi 3, 00166 Rome, Italy. * Corresponding author. Tel.: +421-944624921. E-mail: saeid.okhravi@savba.sk

Abstract

This study aimed to comprehensively investigate the influence of substrate level difference and material composition on dam break wave evolution over two different erodible beds. Utilizing the Volume of Fluid (VOF) method, we tracked free surface advection and reproduced wave evolution using experimental data from the literature. For model validation, a comprehensive sensitivity analysis encompassed mesh resolution, turbulence simulation methods, and bed load transport equations. The implementation of Large Eddy Simulation (LES), non-equilibrium sediment flux, and van Rijn’s (1984) bed load formula yielded higher accuracy compared to alternative approaches. The findings emphasize the significant effect of substrate level difference and material composition on dam break morphodynamic characteristics. Decreasing substrate level disparity led to reduced flow velocity, wavefront progression, free surface height, substrate erosion, and other pertinent parameters. Initial air entrapment proved substantial at the wavefront, illustrating pronounced air-water interaction along the bottom interface. The Shields parameter experienced a one-third reduction as substrate level difference quadrupled, with the highest near-bed concentration observed at the wavefront. This research provides fresh insights into the complex interplay of factors governing dam break wave propagation and morphological changes, advancing our comprehension of this intricate phenomenon.

이 연구는 두 개의 서로 다른 침식층에 대한 댐 파괴파 진화에 대한 기질 수준 차이와 재료 구성의 영향을 종합적으로 조사하는 것을 목표로 했습니다. VOF(유체량) 방법을 활용하여 자유 표면 이류를 추적하고 문헌의 실험 데이터를 사용하여 파동 진화를 재현했습니다.

모델 검증을 위해 메쉬 해상도, 난류 시뮬레이션 방법 및 침대 하중 전달 방정식을 포함하는 포괄적인 민감도 분석을 수행했습니다. LES(Large Eddy Simulation), 비평형 퇴적물 플럭스 및 van Rijn(1984)의 하상 부하 공식의 구현은 대체 접근 방식에 비해 더 높은 정확도를 산출했습니다.

연구 결과는 댐 붕괴 형태역학적 특성에 대한 기질 수준 차이와 재료 구성의 중요한 영향을 강조합니다. 기판 수준 차이가 감소하면 유속, 파면 진행, 자유 표면 높이, 기판 침식 및 기타 관련 매개변수가 감소했습니다.

초기 공기 포집은 파면에서 상당한 것으로 입증되었으며, 이는 바닥 경계면을 따라 뚜렷한 공기-물 상호 작용을 보여줍니다. 기판 레벨 차이가 4배로 증가함에 따라 Shields 매개변수는 1/3로 감소했으며, 파면에서 가장 높은 베드 근처 농도가 관찰되었습니다.

이 연구는 댐 파괴파 전파와 형태학적 변화를 지배하는 요인들의 복잡한 상호 작용에 대한 새로운 통찰력을 제공하여 이 복잡한 현상에 대한 이해를 향상시킵니다.

Keywords

Dam break; Substrate level difference; Erodible bed; Sediment transport; Computational fluid dynamics CFD.

Fig. 3. Free surface and substrate profiles in all Sp and Ls cases at t = 1 s, t = 3 s, and t = 5 s, arranged left to right (note: the colour contours
correspond to the horizontal component of the flow velocity (u), expressed in m/s).
Fig. 3. Free surface and substrate profiles in all Sp and Ls cases at t = 1 s, t = 3 s, and t = 5 s, arranged left to right (note: the colour contours correspond to the horizontal component of the flow velocity (u), expressed in m/s).

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Figure 1 | Schematic of the present research model with dimensions and macro-roughnesses installed.

On the hydraulic performance of the inclined drops: the effect of downstreammacro-roughness elements

경사 낙하의 수력학적 성능: 하류 거시 거칠기 요소의 영향

Farhoud Kalateh a,*, Ehsan Aminvash a and Rasoul Daneshfaraz b
a Faculty of Civil Engineering, University of Tabriz, Tabriz, Iran
b Faculty of Engineering, University of Maragheh, Maragheh, Iran
*Corresponding author. E-mail: f.kalateh@gmail.com

ABSTRACT

The main goal of the present study is to investigate the effects of macro-roughnesses downstream of the inclined drop through numerical models. Due to the vital importance of geometrical properties of the macro-roughnesses in the hydraulic performance and efficient energy dissipation downstream of inclined drops, two different geometries of macro-roughnesses, i.e., semi-circular and triangular geometries, have been investigated using the Flow-3D model. Numerical simulation showed that with the flow rate increase and relative critical depth, the flow energy consumption has decreased. Also, relative energy dissipation increases with the increase in height and slope angle, so that this amount of increase in energy loss compared to the smooth bed in semi-circular and triangular elements is 86.39 and 76.80%, respectively, in the inclined drop with a height of 15 cm and 86.99 and 65.78% in the drop with a height of 20 cm. The Froude number downstream on the uneven bed has been dramatically reduced, so this amount of reduction has been approximately 47 and 54% compared to the control condition. The relative depth of the downstream has also increased due to the turbulence of the flow on the uneven bed with the increase in the flow rate.

본 연구의 주요 목표는 수치 모델을 통해 경사 낙하 하류의 거시 거칠기 효과를 조사하는 것입니다. 수력학적 성능과 경사 낙하 하류의 효율적인 에너지 소산에서 거시 거칠기의 기하학적 특성이 매우 중요하기 때문에 두 가지 서로 다른 거시 거칠기 형상, 즉 반원형 및 삼각형 형상이 Flow를 사용하여 조사되었습니다.

3D 모델 수치 시뮬레이션을 통해 유량이 증가하고 상대 임계 깊이가 증가함에 따라 유동 에너지 소비가 감소하는 것으로 나타났습니다. 또한, 높이와 경사각이 증가함에 따라 상대적인 에너지 소산도 증가하는데, 반원형 요소와 삼각형 요소에서 평활층에 비해 에너지 손실의 증가량은 경사낙하에서 각각 86.39%와 76.80%입니다.

높이 15cm, 높이 20cm의 드롭에서 86.99%, 65.78%입니다. 고르지 못한 베드 하류의 프루드 수가 극적으로 감소하여 이 감소량은 대조 조건에 비해 약 47%와 54%였습니다. 유속이 증가함에 따라 고르지 못한 층에서의 흐름의 난류로 인해 하류의 상대적 깊이도 증가했습니다.

Key words

flow energy dissipation, Froude number, inclined drop, numerical simulation

Figure 1 | Schematic of the present research model with dimensions and macro-roughnesses installed.
Figure 1 | Schematic of the present research model with dimensions and macro-roughnesses installed.
Figure 2 | Meshing, boundary condition, and solution field network
Figure 2 | Meshing, boundary condition, and solution field network

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Fig. 9 From: An Investigation on Hydraulic Aspects of Rectangular Labyrinth Pool and Weir Fishway Using FLOW-3D

An Investigation on Hydraulic Aspects of Rectangular Labyrinth Pool and Weir Fishway Using FLOW-3D

Abstract

웨어의 두 가지 서로 다른 배열(즉, 직선형 웨어와 직사각형 미로 웨어)을 사용하여 웨어 모양, 웨어 간격, 웨어의 오리피스 존재, 흐름 영역에 대한 바닥 경사와 같은 기하학적 매개변수의 영향을 평가했습니다.

유량과 수심의 관계, 수심 평균 속도의 변화와 분포, 난류 특성, 어도에서의 에너지 소산. 흐름 조건에 미치는 영향을 조사하기 위해 FLOW-3D® 소프트웨어를 사용하여 전산 유체 역학 시뮬레이션을 수행했습니다.

수치 모델은 계산된 표면 프로파일과 속도를 문헌의 실험적으로 측정된 값과 비교하여 검증되었습니다. 수치 모델과 실험 데이터의 결과, 급락유동의 표면 프로파일과 표준화된 속도 프로파일에 대한 평균 제곱근 오차와 평균 절대 백분율 오차가 각각 0.014m와 3.11%로 나타나 수치 모델의 능력을 확인했습니다.

수영장과 둑의 흐름 특성을 예측합니다. 각 모델에 대해 L/B = 1.83(L: 웨어 거리, B: 수로 폭) 값에서 급락 흐름이 발생할 수 있고 L/B = 0.61에서 스트리밍 흐름이 발생할 수 있습니다. 직사각형 미로보 모델은 기존 모델보다 무차원 방류량(Q+)이 더 큽니다.

수중 흐름의 기존 보와 직사각형 미로 보의 경우 Q는 각각 1.56과 1.47h에 비례합니다(h: 보 위 수심). 기존 웨어의 풀 내 평균 깊이 속도는 직사각형 미로 웨어의 평균 깊이 속도보다 높습니다.

그러나 주어진 방류량, 바닥 경사 및 웨어 간격에 대해 난류 운동 에너지(TKE) 및 난류 강도(TI) 값은 기존 웨어에 비해 직사각형 미로 웨어에서 더 높습니다. 기존의 웨어는 직사각형 미로 웨어보다 에너지 소산이 더 낮습니다.

더 낮은 TKE 및 TI 값은 미로 웨어 상단, 웨어 하류 벽 모서리, 웨어 측벽과 채널 벽 사이에서 관찰되었습니다. 보와 바닥 경사면 사이의 거리가 증가함에 따라 평균 깊이 속도, 난류 운동 에너지의 평균값 및 난류 강도가 증가하고 수영장의 체적 에너지 소산이 감소했습니다.

둑에 개구부가 있으면 평균 깊이 속도와 TI 값이 증가하고 풀 내에서 가장 높은 TKE 범위가 감소하여 두 모델 모두에서 물고기를 위한 휴식 공간이 더 넓어지고(TKE가 낮아짐) 에너지 소산율이 감소했습니다.

Two different arrangements of the weir (i.e., straight weir and rectangular labyrinth weir) were used to evaluate the effects of geometric parameters such as weir shape, weir spacing, presence of an orifice at the weir, and bed slope on the flow regime and the relationship between discharge and depth, variation and distribution of depth-averaged velocity, turbulence characteristics, and energy dissipation at the fishway. Computational fluid dynamics simulations were performed using FLOW-3D® software to examine the effects on flow conditions. The numerical model was validated by comparing the calculated surface profiles and velocities with experimentally measured values from the literature. The results of the numerical model and experimental data showed that the root-mean-square error and mean absolute percentage error for the surface profiles and normalized velocity profiles of plunging flows were 0.014 m and 3.11%, respectively, confirming the ability of the numerical model to predict the flow characteristics of the pool and weir. A plunging flow can occur at values of L/B = 1.83 (L: distance of the weir, B: width of the channel) and streaming flow at L/B = 0.61 for each model. The rectangular labyrinth weir model has larger dimensionless discharge values (Q+) than the conventional model. For the conventional weir and the rectangular labyrinth weir at submerged flow, Q is proportional to 1.56 and 1.47h, respectively (h: the water depth above the weir). The average depth velocity in the pool of a conventional weir is higher than that of a rectangular labyrinth weir. However, for a given discharge, bed slope, and weir spacing, the turbulent kinetic energy (TKE) and turbulence intensity (TI) values are higher for a rectangular labyrinth weir compared to conventional weir. The conventional weir has lower energy dissipation than the rectangular labyrinth weir. Lower TKE and TI values were observed at the top of the labyrinth weir, at the corner of the wall downstream of the weir, and between the side walls of the weir and the channel wall. As the distance between the weirs and the bottom slope increased, the average depth velocity, the average value of turbulent kinetic energy and the turbulence intensity increased, and the volumetric energy dissipation in the pool decreased. The presence of an opening in the weir increased the average depth velocity and TI values and decreased the range of highest TKE within the pool, resulted in larger resting areas for fish (lower TKE), and decreased the energy dissipation rates in both models.

1 Introduction

Artificial barriers such as detour dams, weirs, and culverts in lakes and rivers prevent fish from migrating and completing the upstream and downstream movement cycle. This chain is related to the life stage of the fish, its location, and the type of migration. Several riverine fish species instinctively migrate upstream for spawning and other needs. Conversely, downstream migration is a characteristic of early life stages [1]. A fish ladder is a waterway that allows one or more fish species to cross a specific obstacle. These structures are constructed near detour dams and other transverse structures that have prevented such migration by allowing fish to overcome obstacles [2]. The flow pattern in fish ladders influences safe and comfortable passage for ascending fish. The flow’s strong turbulence can reduce the fish’s speed, injure them, and delay or prevent them from exiting the fish ladder. In adult fish, spawning migrations are usually complex, and delays are critical to reproductive success [3].

Various fish ladders/fishways include vertical slots, denil, rock ramps, and pool weirs [1]. The choice of fish ladder usually depends on many factors, including water elevation, space available for construction, and fish species. Pool and weir structures are among the most important fish ladders that help fish overcome obstacles in streams or rivers and swim upstream [1]. Because they are easy to construct and maintain, this type of fish ladder has received considerable attention from researchers and practitioners. Such a fish ladder consists of a sloping-floor channel with series of pools directly separated by a series of weirs [4]. These fish ladders, with or without underwater openings, are generally well-suited for slopes of 10% or less [12]. Within these pools, flow velocities are low and provide resting areas for fish after they enter the fish ladder. After resting in the pools, fish overcome these weirs by blasting or jumping over them [2]. There may also be an opening in the flooded portion of the weir through which the fish can swim instead of jumping over the weir. Design parameters such as the length of the pool, the height of the weir, the slope of the bottom, and the water discharge are the most important factors in determining the hydraulic structure of this type of fish ladder [3]. The flow over the weir depends on the flow depth at a given slope S0 and the pool length, either “plunging” or “streaming.” In plunging flow, the water column h over each weir creates a water jet that releases energy through turbulent mixing and diffusion mechanisms [5]. The dimensionless discharges for plunging (Q+) and streaming (Q*) flows are shown in Fig. 1, where Q is the total discharge, B is the width of the channel, w is the weir height, S0 is the slope of the bottom, h is the water depth above the weir, d is the flow depth, and g is the acceleration due to gravity. The maximum velocity occurs near the top of the weir for plunging flow. At the water’s surface, it drops to about half [6].

figure 1
Fig. 1

Extensive experimental studies have been conducted to investigate flow patterns for various physical geometries (i.e., bed slope, pool length, and weir height) [2]. Guiny et al. [7] modified the standard design by adding vertical slots, orifices, and weirs in fishways. The efficiency of the orifices and vertical slots was related to the velocities at their entrances. In the laboratory experiments of Yagci [8], the three-dimensional (3D) mean flow and turbulence structure of a pool weir fishway combined with an orifice and a slot is investigated. It is shown that the energy dissipation per unit volume and the discharge have a linear relationship.

Considering the beneficial characteristics reported in the limited studies of researchers on the labyrinth weir in the pool-weir-type fishway, and knowing that the characteristics of flow in pool-weir-type fishways are highly dependent on the geometry of the weir, an alternative design of the rectangular labyrinth weir instead of the straight weirs in the pool-weir-type fishway is investigated in this study [79]. Kim [10] conducted experiments to compare the hydraulic characteristics of three different weir types in a pool-weir-type fishway. The results show that a straight, rectangular weir with a notch is preferable to a zigzag or trapezoidal weir. Studies on natural fish passes show that pass ability can be improved by lengthening the weir’s crest [7]. Zhong et al. [11] investigated the semi-rigid weir’s hydraulic performance in the fishway’s flow field with a pool weir. The results showed that this type of fishway performed better with a lower invert slope and a smaller radius ratio but with a larger pool spacing.

Considering that an alternative method to study the flow characteristics in a fishway with a pool weir is based on numerical methods and modeling from computational fluid dynamics (CFD), which can easily change the geometry of the fishway for different flow fields, this study uses the powerful package CFD and the software FLOW-3D to evaluate the proposed weir design and compare it with the conventional one to extend the application of the fishway. The main objective of this study was to evaluate the hydraulic performance of the rectangular labyrinth pool and the weir with submerged openings in different hydraulic configurations. The primary objective of creating a new weir configuration for suitable flow patterns is evaluated based on the swimming capabilities of different fish species. Specifically, the following questions will be answered: (a) How do the various hydraulic and geometric parameters relate to the effects of water velocity and turbulence, expressed as turbulent kinetic energy (TKE) and turbulence intensity (TI) within the fishway, i.e., are conventional weirs more affected by hydraulics than rectangular labyrinth weirs? (b) Which weir configurations have the greatest effect on fish performance in the fishway? (c) In the presence of an orifice plate, does the performance of each weir configuration differ with different weir spacing, bed gradients, and flow regimes from that without an orifice plate?

2 Materials and Methods

2.1 Physical Model Configuration

This paper focuses on Ead et al. [6]’s laboratory experiments as a reference, testing ten pool weirs (Fig. 2). The experimental flume was 6 m long, 0.56 m wide, and 0.6 m high, with a bottom slope of 10%. Field measurements were made at steady flow with a maximum flow rate of 0.165 m3/s. Discharge was measured with magnetic flow meters in the inlets and water level with point meters (see Ead et al. [6]. for more details). Table 1 summarizes the experimental conditions considered for model calibration in this study.

figure 2
Fig. 2

Table 1 Experimental conditions considered for calibration

Full size table

2.2 Numerical Models

Computational fluid dynamics (CFD) simulations were performed using FLOW-3D® v11.2 to validate a series of experimental liner pool weirs by Ead et al. [6] and to investigate the effects of the rectangular labyrinth pool weir with an orifice. The dimensions of the channel and data collection areas in the numerical models are the same as those of the laboratory model. Two types of pool weirs were considered: conventional and labyrinth. The proposed rectangular labyrinth pool weirs have a symmetrical cross section and are sized to fit within the experimental channel. The conventional pool weir model had a pool length of l = 0.685 and 0.342 m, a weir height of w = 0.141 m, a weir width of B = 0.56 m, and a channel slope of S0 = 5 and 10%. The rectangular labyrinth weirs have the same front width as the offset, i.e., a = b = c = 0.186 m. A square underwater opening with a width of 0.05 m and a depth of 0.05 m was created in the middle of the weir. The weir configuration considered in the present study is shown in Fig. 3.

figure 3
Fig. 3

2.3 Governing Equations

FLOW-3D® software solves the Navier–Stokes–Reynolds equations for three-dimensional analysis of incompressible flows using the fluid-volume method on a gridded domain. FLOW -3D® uses an advanced free surface flow tracking algorithm (TruVOF) developed by Hirt and Nichols [12], where fluid configurations are defined in terms of a VOF function F (xyzt). In this case, F (fluid fraction) represents the volume fraction occupied by the fluid: F = 1 in cells filled with fluid and F = 0 in cells without fluid (empty areas) [413]. The free surface area is at an intermediate value of F. (Typically, F = 0.5, but the user can specify a different intermediate value.) The equations in Cartesian coordinates (xyz) applicable to the model are as follows:

�f∂�∂�+∂(���x)∂�+∂(���y)∂�+∂(���z)∂�=�SOR

(1)

∂�∂�+1�f(��x∂�∂�+��y∂�∂�+��z∂�∂�)=−1�∂�∂�+�x+�x

(2)

∂�∂�+1�f(��x∂�∂�+��y∂�∂�+��z∂�∂�)=−1�∂�∂�+�y+�y

(3)

∂�∂�+1�f(��x∂�∂�+��y∂�∂�+��z∂�∂�)=−1�∂�∂�+�z+�z

(4)

where (uvw) are the velocity components, (AxAyAz) are the flow area components, (Gx, Gy, Gz) are the mass accelerations, and (fxfyfz) are the viscous accelerations in the directions (xyz), ρ is the fluid density, RSOR is the spring term, Vf is the volume fraction associated with the flow, and P is the pressure. The kε turbulence model (RNG) was used in this study to solve the turbulence of the flow field. This model is a modified version of the standard kε model that improves performance. The model is a two-equation model; the first equation (Eq. 5) expresses the turbulence’s energy, called turbulent kinetic energy (k) [14]. The second equation (Eq. 6) is the turbulent dissipation rate (ε), which determines the rate of dissipation of kinetic energy [15]. These equations are expressed as follows Dasineh et al. [4]:

∂(��)∂�+∂(����)∂��=∂∂��[������∂�∂��]+��−�ε

(5)

∂(�ε)∂�+∂(�ε��)∂��=∂∂��[�ε�eff∂ε∂��]+�1εε��k−�2ε�ε2�

(6)

In these equations, k is the turbulent kinetic energy, ε is the turbulent energy consumption rate, Gk is the generation of turbulent kinetic energy by the average velocity gradient, with empirical constants αε = αk = 1.39, C1ε = 1.42, and C2ε = 1.68, eff is the effective viscosity, μeff = μ + μt [15]. Here, μ is the hydrodynamic density coefficient, and μt is the turbulent density of the fluid.

2.4 Meshing and the Boundary Conditions in the Model Setup

The numerical area is divided into three mesh blocks in the X-direction. The meshes are divided into different sizes, a containing mesh block for the entire spatial domain and a nested block with refined cells for the domain of interest. Three different sizes were selected for each of the grid blocks. By comparing the accuracy of their results based on the experimental data, the reasonable mesh for the solution domain was finally selected. The convergence index method (GCI) evaluated the mesh sensitivity analysis. Based on this method, many researchers, such as Ahmadi et al. [16] and Ahmadi et al. [15], have studied the independence of numerical results from mesh size. Three different mesh sizes with a refinement ratio (r) of 1.33 were used to perform the convergence index method. The refinement ratio is the ratio between the larger and smaller mesh sizes (r = Gcoarse/Gfine). According to the recommendation of Celik et al. [17], the recommended number for the refinement ratio is 1.3, which gives acceptable results. Table 2 shows the characteristics of the three mesh sizes selected for mesh sensitivity analysis.Table 2 Characteristics of the meshes tested in the convergence analysis

Full size table

The results of u1 = umax (u1 = velocity component along the x1 axis and umax = maximum velocity of u1 in a section perpendicular to the invert of the fishway) at Q = 0.035 m3/s, × 1/l = 0.66, and Y1/b = 0 in the pool of conventional weir No. 4, obtained from the output results of the software, were used to evaluate the accuracy of the calculation range. As shown in Fig. 4x1 = the distance from a given weir in the x-direction, Y1 = the water depth measured in the y-direction, Y0 = the vertical distance in the Cartesian coordinate system, h = the water column at the crest, b = the distance between the two points of maximum velocity umax and zero velocity, and l = the pool length.

figure 4
Fig. 4

The apparent index of convergence (p) in the GCI method is calculated as follows:

�=ln⁡(�3−�2)(�2−�1)/ln⁡(�)

(7)

f1f2, and f3 are the hydraulic parameters obtained from the numerical simulation (f1 corresponds to the small mesh), and r is the refinement ratio. The following equation defines the convergence index of the fine mesh:

GCIfine=1.25|ε|��−1

(8)

Here, ε = (f2 − f1)/f1 is the relative error, and f2 and f3 are the values of hydraulic parameters considered for medium and small grids, respectively. GCI12 and GCI23 dimensionless indices can be calculated as:

GCI12=1.25|�2−�1�1|��−1

(9)

Then, the independence of the network is preserved. The convergence index of the network parameters obtained by Eqs. (7)–(9) for all three network variables is shown in Table 3. Since the GCI values for the smaller grid (GCI12) are lower compared to coarse grid (GCI23), it can be concluded that the independence of the grid is almost achieved. No further change in the grid size of the solution domain is required. The calculated values (GCI23/rpGCI12) are close to 1, which shows that the numerical results obtained are within the convergence range. As a result, the meshing of the solution domain consisting of a block mesh with a mesh size of 0.012 m and a block mesh within a larger block mesh with a mesh size of 0.009 m was selected as the optimal mesh (Fig. 5).Table 3 GCI calculation

Full size table

figure 5
Fig. 5

The boundary conditions applied to the area are shown in Fig. 6. The boundary condition of specific flow rate (volume flow rate-Q) was used for the inlet of the flow. For the downstream boundary, the flow output (outflow-O) condition did not affect the flow in the solution area. For the Zmax boundary, the specified pressure boundary condition was used along with the fluid fraction = 0 (P). This type of boundary condition considers free surface or atmospheric pressure conditions (Ghaderi et al. [19]). The wall boundary condition is defined for the bottom of the channel, which acts like a virtual wall without friction (W). The boundary between mesh blocks and walls were considered a symmetrical condition (S).

figure 6
Fig. 6

The convergence of the steady-state solutions was controlled during the simulations by monitoring the changes in discharge at the inlet boundary conditions. Figure 7 shows the time series plots of the discharge obtained from the Model A for the three main discharges from the numerical results. The 8 s to reach the flow equilibrium is suitable for the case of the fish ladder with pool and weir. Almost all discharge fluctuations in the models are insignificant in time, and the flow has reached relative stability. The computation time for the simulations was between 6 and 8 h using a personal computer with eight cores of a CPU (Intel Core i7-7700K @ 4.20 GHz and 16 GB RAM).

figure 7
Fig. 7

3 Results

3.1 Verification of Numerical Results

Quantitative outcomes, including free surface and normalized velocity profiles obtained using FLOW-3D software, were reviewed and compared with the results of Ead et al. [6]. The fourth pool was selected to present the results and compare the experiment and simulation. For each quantity, the percentage of mean absolute error (MAPE (%)) and root-mean-square error (RMSE) are calculated. Equations (10) and (11) show the method used to calculate the errors.

MAPE(%)100×1�∑1�|�exp−�num�exp|

(10)

RMSE(−)1�∑1�(�exp−�num)2

(11)

Here, Xexp is the value of the laboratory data, Xnum is the numerical data value, and n is the amount of data. As shown in Fig. 8, let x1 = distance from a given weir in the x-direction and Y1 = water depth in the y-direction from the bottom. The trend of the surface profiles for each of the numerical results is the same as that of the laboratory results. The surface profiles of the plunging flows drop after the flow enters and then rises to approach the next weir. The RMSE and MAPE error values for Model A are 0.014 m and 3.11%, respectively, indicating acceptable agreement between numerical and laboratory results. Figure 9 shows the velocity vectors and plunging flow from the numerical results, where x and y are horizontal and vertical to the flow direction, respectively. It can be seen that the jet in the fish ladder pool has a relatively high velocity. The two vortices, i.e., the enclosed vortex rotating clockwise behind the weir and the surface vortex rotating counterclockwise above the jet, are observed for the regime of incident flow. The point where the jet meets the fish passage bed is shown in the figure. The normalized velocity profiles upstream and downstream of the impact points are shown in Fig. 10. The figure shows that the numerical results agree well with the experimental data of Ead et al. [6].

figure 8
Fig. 8
figure 9
Fig. 9
figure 10
Fig. 10

3.2 Flow Regime and Discharge-Depth Relationship

Depending on the geometric shape of the fishway, including the distance of the weir, the slope of the bottom, the height of the weir, and the flow conditions, the flow regime in the fishway is divided into three categories: dipping, transitional, and flow regimes [4]. In the plunging flow regime, the flow enters the pool through the weir, impacts the bottom of the fishway, and forms a hydraulic jump causing two eddies [220]. In the streamwise flow regime, the surface of the flow passing over the weir is almost parallel to the bottom of the channel. The transitional regime has intermediate flow characteristics between the submerged and flow regimes. To predict the flow regime created in the fishway, Ead et al. [6] proposed two dimensionless parameters, Qt* and L/w, where Qt* is the dimensionless discharge, L is the distance between weirs, and w is the height of the weir:

��∗=���0���

(12)

Q is the total discharge, B is the width of the channel, S0 is the slope of the bed, and g is the gravity acceleration. Figure 11 shows different ranges for each flow regime based on the slope of the bed and the distance between the pools in this study. The results of Baki et al. [21], Ead et al. [6] and Dizabadi et al. [22] were used for this comparison. The distance between the pools affects the changes in the regime of the fish ladder. So, if you decrease the distance between weirs, the flow regime more likely becomes. This study determined all three flow regimes in a fish ladder. When the corresponding range of Qt* is less than 0.6, the flow regime can dip at values of L/B = 1.83. If the corresponding range of Qt* is greater than 0.5, transitional flow may occur at L/B = 1.22. On the other hand, when Qt* is greater than 1, streamwise flow can occur at values of L/B = 0.61. These observations agree well with the results of Baki et al. [21], Ead et al. [6] and Dizabadi et al. [22].

figure 11
Fig. 11

For plunging flows, another dimensionless discharge (Q+) versus h/w given by Ead et al. [6] was used for further evaluation:

�+=��ℎ�ℎ=23�d�

(13)

where h is the water depth above the weir, and Cd is the discharge coefficient. Figure 12a compares the numerical and experimental results of Ead et al. [6]. In this figure, Rehbock’s empirical equation is used to estimate the discharge coefficient of Ead et al. [6].

�d=0.57+0.075ℎ�

(14)

figure 12
Fig. 12

The numerical results for the conventional weir (Model A) and the rectangular labyrinth weir (Model B) of this study agree well with the laboratory results of Ead et al. [6]. When comparing models A and B, it is also found that a rectangular labyrinth weir has larger Q + values than the conventional weir as the length of the weir crest increases for a given channel width and fixed headwater elevation. In Fig. 12b, Models A and B’s flow depth plot shows the plunging flow regime. The power trend lines drawn through the data are the best-fit lines. The data shown in Fig. 12b are for different bed slopes and weir geometries. For the conventional weir and the rectangular labyrinth weir at submerged flow, Q can be assumed to be proportional to 1.56 and 1.47h, respectively. In the results of Ead et al. [6], Q is proportional to 1.5h. If we assume that the flow through the orifice is Qo and the total outflow is Q, the change in the ratio of Qo/Q to total outflow for models A and B can be shown in Fig. 13. For both models, the flow through the orifice decreases as the total flow increases. A logarithmic trend line was also found between the total outflow and the dimensionless ratio Qo/Q.

figure 13
Fig. 13

3.3 Depth-Averaged Velocity Distributions

To ensure that the target fish species can pass the fish ladder with maximum efficiency, the average velocity in the fish ladder should be low enough [4]. Therefore, the average velocity in depth should be as much as possible below the critical swimming velocities of the target fishes at a constant flow depth in the pool [20]. The contour plot of depth-averaged velocity was used instead of another direction, such as longitudinal velocity because fish are more sensitive to depth-averaged flow velocity than to its direction under different hydraulic conditions. Figure 14 shows the distribution of depth-averaged velocity in the pool for Models A and B in two cases with and without orifice plates. Model A’s velocity within the pool differs slightly in the spanwise direction. However, no significant variation in velocity was observed. The flow is gradually directed to the sides as it passes through the rectangular labyrinth weir. This increases the velocity at the sides of the channel. Therefore, the high-velocity zone is located at the sides. The low velocity is in the downstream apex of the weir. This area may be suitable for swimming target fish. The presence of an opening in the weir increases the flow velocity at the opening and in the pool’s center, especially in Model A. The flow velocity increase caused by the models’ opening varied from 7.7 to 12.48%. Figure 15 illustrates the effect of the inverted slope on the averaged depth velocity distribution in the pool at low and high discharge. At constant discharge, flow velocity increases with increasing bed slope. In general, high flow velocity was found in the weir toe sidewall and the weir and channel sidewalls.

figure 14
Fig. 14
figure 15
Fig. 15

On the other hand, for a constant bed slope, the high-velocity area of the pool increases due to the increase in runoff. For both bed slopes and different discharges, the most appropriate path for fish to travel from upstream to downstream is through the middle of the cross section and along the top of the rectangular labyrinth weirs. The maximum dominant velocities for Model B at S0 = 5% were 0.83 and 1.01 m/s; at S0 = 10%, they were 1.12 and 1.61 m/s at low and high flows, respectively. The low mean velocities for the same distance and S0 = 5 and 10% were 0.17 and 0.26 m/s, respectively.

Figure 16 shows the contour of the averaged depth velocity for various distances from the weir at low and high discharge. The contour plot shows a large variation in velocity within short distances from the weir. At L/B = 0.61, velocities are low upstream and downstream of the top of the weir. The high velocities occur in the side walls of the weir and the channel. At L/B = 1.22, the low-velocity zone displaces the higher velocity in most of the pool. Higher velocities were found only on the sides of the channel. As the discharge increases, the velocity zone in the pool becomes wider. At L/B = 1.83, there is an area of higher velocities only upstream of the crest and on the sides of the weir. At high discharge, the prevailing maximum velocities for L/B = 0.61, 1.22, and 1.83 were 1.46, 1.65, and 1.84 m/s, respectively. As the distance between weirs increases, the range of maximum velocity increases.

figure 16
Fig. 16

On the other hand, the low mean velocity for these distances was 0.27, 0.44, and 0.72 m/s, respectively. Thus, the low-velocity zone decreases with increasing distance between weirs. Figure 17 shows the pattern distribution of streamlines along with the velocity contour at various distances from the weir for Q = 0.05 m3/s. A stream-like flow is generally formed in the pool at a small distance between weirs (L/B = 0.61). The rotation cell under the jet forms clockwise between the two weirs. At the distances between the spillways (L/B = 1.22), the transition regime of the flow is formed. The transition regime occurs when or shortly after the weir is flooded. The rotation cell under the jet is clockwise smaller than the flow regime and larger than the submergence regime. At a distance L/B = 1.83, a plunging flow is formed so that the plunging jet dips into the pool and extends downstream to the center of the pool. The clockwise rotation of the cell is bounded by the dipping jet of the weir and is located between the bottom and the side walls of the weir and the channel.

figure 17
Fig. 17

Figure 18 shows the average depth velocity bar graph for each weir at different bed slopes and with and without orifice plates. As the distance between weirs increases, all models’ average depth velocity increases. As the slope of the bottom increases and an orifice plate is present, the average depth velocity in the pool increases. In addition, the average pool depth velocity increases as the discharge increases. Among the models, Model A’s average depth velocity is higher than Model B’s. The variation in velocity ranged from 8.11 to 12.24% for the models without an orifice plate and from 10.26 to 16.87% for the models with an orifice plate.

figure 18
Fig. 18

3.4 Turbulence Characteristics

The turbulent kinetic energy is one of the important parameters reflecting the turbulent properties of the flow field [23]. When the k value is high, more energy and a longer transit time are required to migrate the target species. The turbulent kinetic energy is defined as follows:

�=12(�x′2+�y′2+�z′2)

(15)

where uxuy, and uz are fluctuating velocities in the xy, and z directions, respectively. An illustration of the TKE and the effects of the geometric arrangement of the weir and the presence of an opening in the weir is shown in Fig. 19. For a given bed slope, in Model A, the highest TKE values are uniformly distributed in the weir’s upstream portion in the channel’s cross section. In contrast, for the rectangular labyrinth weir (Model B), the highest TKE values are concentrated on the sides of the pool between the crest of the weir and the channel wall. The highest TKE value in Models A and B is 0.224 and 0.278 J/kg, respectively, at the highest bottom slope (S0 = 10%). In the downstream portion of the conventional weir and within the crest of the weir and the walls of the rectangular labyrinth, there was a much lower TKE value that provided the best conditions for fish to recover in the pool between the weirs. The average of the lowest TKE for bottom slopes of 5 and 10% in Model A is 0.041 and 0.056 J/kg, and for Model B, is 0.047 and 0.064 J/kg. The presence of an opening in the weirs reduces the area of the highest TKE within the pool. It also increases the resting areas for fish (lower TKE). The highest TKE at the highest bottom slope in Models A and B with an orifice is 0.208 and 0.191 J/kg, respectively.

figure 19
Fig. 19

Figure 20 shows the effect of slope on the longitudinal distribution of TKE in the pools. TKE values significantly increase for a given discharge with an increasing bottom slope. Thus, for a low bed slope (S0 = 5%), a large pool area has expanded with average values of 0.131 and 0.168 J/kg for low and high discharge, respectively. For a bed slope of S0 = 10%, the average TKE values are 0.176 and 0.234 J/kg. Furthermore, as the discharge increases, the area with high TKE values within the pool increases. Lower TKE values are observed at the apex of the labyrinth weir, at the corner of the wall downstream of the weir, and between the side walls of the weir and the channel wall for both bottom slopes. The effect of distance between weirs on TKE is shown in Fig. 21. Low TKE values were observed at low discharge and short distances between weirs. Low TKE values are located at the top of the rectangular labyrinth weir and the downstream corner of the weir wall. There is a maximum value of TKE at the large distances between weirs, L/B = 1.83, along the center line of the pool, where the dip jet meets the bottom of the bed. At high discharge, the maximum TKE value for the distance L/B = 0.61, 1.22, and 1.83 was 0.246, 0.322, and 0.417 J/kg, respectively. In addition, the maximum TKE range increases with the distance between weirs.

figure 20
Fig. 20
figure 21
Fig. 21

For TKE size, the average value (TKEave) is plotted against q in Fig. 22. For all models, the TKE values increase with increasing q. For example, in models A and B with L/B = 0.61 and a slope of 10%, the TKE value increases by 41.66 and 86.95%, respectively, as q increases from 0.1 to 0.27 m2/s. The TKE values in Model B are higher than Model A for a given discharge, bed slope, and weir distance. The TKEave in Model B is higher compared to Model A, ranging from 31.46 to 57.94%. The presence of an orifice in the weir reduces the TKE values in both weirs. The intensity of the reduction is greater in Model B. For example, in Models A and B with L/B = 0.61 and q = 0.1 m2/s, an orifice reduces TKEave values by 60.35 and 19.04%, respectively. For each model, increasing the bed slope increases the TKEave values in the pool. For example, for Model B with q = 0.18 m2/s, increasing the bed slope from 5 to 10% increases the TKEave value by 14.34%. Increasing the distance between weirs increases the TKEave values in the pool. For example, in Model B with S0 = 10% and q = 0.3 m2/s, the TKEave in the pool increases by 34.22% if you increase the distance between weirs from L/B = 0.61 to L/B = 0.183.

figure 22
Fig. 22

Cotel et al. [24] suggested that turbulence intensity (TI) is a suitable parameter for studying fish swimming performance. Figure 23 shows the plot of TI and the effects of the geometric arrangement of the weir and the presence of an orifice. In Model A, the highest TI values are found upstream of the weirs and are evenly distributed across the cross section of the channel. The TI values increase as you move upstream to downstream in the pool. For the rectangular labyrinth weir, the highest TI values were concentrated on the sides of the pool, between the top of the weir and the side wall of the channel, and along the top of the weir. Downstream of the conventional weir, within the apex of the weir, and at the corners of the walls of the rectangular labyrinth weir, the percentage of TI was low. At the highest discharge, the average range of TI in Models A and B was 24–45% and 15–62%, respectively. The diversity of TI is greater in the rectangular labyrinth weir than the conventional weir. Fish swimming performance is reduced due to higher turbulence intensity. However, fish species may prefer different disturbance intensities depending on their swimming abilities; for example, Salmo trutta prefers a disturbance intensity of 18–53% [25]. Kupferschmidt and Zhu [26] found a higher range of TI for fishways, such as natural rock weirs, of 40–60%. The presence of an orifice in the weir increases TI values within the pool, especially along the middle portion of the cross section of the fishway. With an orifice in the weir, the average range of TI in Models A and B was 28–59% and 22–73%, respectively.

figure 23
Fig. 23

The effect of bed slope on TI variation is shown in Fig. 24. TI increases in different pool areas as the bed slope increases for a given discharge. For a low bed slope (S0 = 5%), a large pool area has increased from 38 to 63% and from 56 to 71% for low and high discharge, respectively. For a bed slope of S0 = 10%, the average values of TI are 45–67% and 61–73% for low and high discharge, respectively. Therefore, as runoff increases, the area with high TI values within the pool increases. A lower TI is observed for both bottom slopes in the corner of the wall, downstream of the crest walls, and between the side walls in the weir and channel. Figure 25 compares weir spacing with the distribution of TI values within the pool. The TI values are low at low flows and short distances between weirs. A maximum value of TI occurs at long spacing and where the plunging stream impinges on the bed and the area around the bed. TI ranges from 36 to 57%, 58–72%, and 47–76% for the highest flow in a wide pool area for L/B = 0.61, 1.22, and 1.83, respectively.

figure 24
Fig. 24
figure 25
Fig. 25

The average value of turbulence intensity (TIave) is plotted against q in Fig. 26. The increase in TI values with the increase in q values is seen in all models. For example, the average values of TI for Models A and B at L/B = 0.61 and slope of 10% increased from 23.9 to 33.5% and from 42 to 51.8%, respectively, with the increase in q from 0.1 to 0.27 m2/s. For a given discharge, a given gradient, and a given spacing of weirs, the TIave is higher in Model B than Model A. The presence of an orifice in the weirs increases the TI values in both types. For example, in Models A and B with L/B = 0.61 and q = 0.1 m2/s, the presence of an orifice increases TIave from 23.9 to 37.1% and from 42 to 48.8%, respectively. For each model, TIave in the pool increases with increasing bed slope. For Model B with q = 0.18 m2/s, TIave increases from 37.5 to 45.8% when you increase the invert slope from 5 to 10%. Increasing the distance between weirs increases the TIave in the pool. In Model B with S0 = 10% and q = 0.3 m2/s, the TIave in the pool increases from 51.8 to 63.7% as the distance between weirs increases from L/B = 0.61 to L/B = 0.183.

figure 26
Fig. 26

3.5 Energy Dissipation

To facilitate the passage of various target species through the pool of fishways, it is necessary to pay attention to the energy dissipation of the flow and to keep the flow velocity in the pool slow. The average volumetric energy dissipation (k) in the pool is calculated using the following basic formula:

�=����0��

(16)

where ρ is the water density, and H is the average water depth of the pool. The change in k versus Q for all models at two bottom slopes, S0 = 5%, and S0 = 10%, is shown in Fig. 27. Like the results of Yagci [8] and Kupferschmidt and Zhu [26], at a constant bottom slope, the energy dissipation in the pool increases with increasing discharge. The trend of change in k as a function of Q from the present study at a bottom gradient of S0 = 5% is also consistent with the results of Kupferschmidt and Zhu [26] for the fishway with rock weir. The only difference between the results is the geometry of the fishway and the combination of boulders instead of a solid wall. Comparison of the models shows that the conventional model has lower energy dissipation than the rectangular labyrinth for a given discharge. Also, increasing the distance between weirs decreases the volumetric energy dissipation for each model with the same bed slope. Increasing the slope of the bottom leads to an increase in volumetric energy dissipation, and an opening in the weir leads to a decrease in volumetric energy dissipation for both models. Therefore, as a guideline for volumetric energy dissipation, if the value within the pool is too high, the increased distance of the weir, the decreased slope of the bed, or the creation of an opening in the weir would decrease the volumetric dissipation rate.

figure 27
Fig. 27

To evaluate the energy dissipation inside the pool, the general method of energy difference in two sections can use:

ε=�1−�2�1

(17)

where ε is the energy dissipation rate, and E1 and E2 are the specific energies in Sects. 1 and 2, respectively. The distance between Sects. 1 and 2 is the same. (L is the distance between two upstream and downstream weirs.) Figure 28 shows the changes in ε relative to q (flow per unit width). The rectangular labyrinth weir (Model B) has a higher energy dissipation rate than the conventional weir (Model A) at a constant bottom gradient. For example, at S0 = 5%, L/B = 0.61, and q = 0.08 m3/s.m, the energy dissipation rate in Model A (conventional weir) was 0.261. In Model B (rectangular labyrinth weir), however, it was 0.338 (22.75% increase). For each model, the energy dissipation rate within the pool increases as the slope of the bottom increases. For Model B with L/B = 1.83 and q = 0.178 m3/s.m, the energy dissipation rate at S0 = 5% and 10% is 0.305 and 0.358, respectively (14.8% increase). Figure 29 shows an orifice’s effect on the pools’ energy dissipation rate. With an orifice in the weir, both models’ energy dissipation rates decreased. Thus, the reduction in energy dissipation rate varied from 7.32 to 9.48% for Model A and from 8.46 to 10.57 for Model B.

figure 28
Fig. 28
figure 29
Fig. 29

4 Discussion

This study consisted of entirely of numerical analysis. Although this study was limited to two weirs, the hydraulic performance and flow characteristics in a pooled fishway are highlighted by the rectangular labyrinth weir and its comparison with the conventional straight weir. The study compared the numerical simulations with laboratory experiments in terms of surface profiles, velocity vectors, and flow characteristics in a fish ladder pool. The results indicate agreement between the numerical and laboratory data, supporting the reliability of the numerical model in capturing the observed phenomena.

When the configuration of the weir changes to a rectangular labyrinth weir, the flow characteristics, the maximum and minimum area, and even the location of each hydraulic parameter change compared to a conventional weir. In the rectangular labyrinth weir, the flow is gradually directed to the sides as it passes the weir. This increases the velocity at the sides of the channel [21]. Therefore, the high-velocity area is located on the sides. In the downstream apex of the weir, the flow velocity is low, and this area may be suitable for swimming target fish. However, no significant change in velocity was observed at the conventional weir within the fish ladder. This resulted in an average increase in TKE of 32% and an average increase in TI of about 17% compared to conventional weirs.

In addition, there is a slight difference in the flow regime for both weir configurations. In addition, the rectangular labyrinth weir has a higher energy dissipation rate for a given discharge and constant bottom slope than the conventional weir. By reducing the distance between the weirs, this becomes even more intense. Finally, the presence of an orifice in both configurations of the weir increased the flow velocity at the orifice and in the middle of the pool, reducing the highest TKE value and increasing the values of TI within the pool of the fish ladder. This resulted in a reduction in volumetric energy dissipation for both weir configurations.

The results of this study will help the reader understand the direct effects of the governing geometric parameters on the hydraulic characteristics of a fishway with a pool and weir. However, due to the limited configurations of the study, further investigation is needed to evaluate the position of the weir’s crest on the flow direction and the difference in flow characteristics when combining boulders instead of a solid wall for this type of labyrinth weir [26]. In addition, hydraulic engineers and biologists must work together to design an effective fishway with rectangular labyrinth configurations. The migration habits of the target species should be considered when designing the most appropriate design [27]. Parametric studies and field observations are recommended to determine the perfect design criteria.

The current study focused on comparing a rectangular labyrinth weir with a conventional straight weir. Further research can explore other weir configurations, such as variations in crest position, different shapes of labyrinth weirs, or the use of boulders instead of solid walls. This would help understand the influence of different geometric parameters on hydraulic characteristics.

5 Conclusions

A new layout of the weir was evaluated, namely a rectangular labyrinth weir compared to a straight weir in a pool and weir system. The differences between the weirs were highlighted, particularly how variations in the geometry of the structures, such as the shape of the weir, the spacing of the weir, the presence of an opening at the weir, and the slope of the bottom, affect the hydraulics within the structures. The main findings of this study are as follows:

  • The calculated dimensionless discharge (Qt*) confirmed three different flow regimes: when the corresponding range of Qt* is smaller than 0.6, the regime of plunging flow occurs for values of L/B = 1.83. (L: distance of the weir; B: channel width). When the corresponding range of Qt* is greater than 0.5, transitional flow occurs at L/B = 1.22. On the other hand, if Qt* is greater than 1, the streaming flow is at values of L/B = 0.61.
  • For the conventional weir and the rectangular labyrinth weir with the plunging flow, it can be assumed that the discharge (Q) is proportional to 1.56 and 1.47h, respectively (h: water depth above the weir). This information is useful for estimating the discharge based on water depth in practical applications.
  • In the rectangular labyrinth weir, the high-velocity zone is located on the side walls between the top of the weir and the channel wall. A high-velocity variation within short distances of the weir. Low velocity occurs within the downstream apex of the weir. This area may be suitable for swimming target fish.
  • As the distance between weirs increased, the zone of maximum velocity increased. However, the zone of low speed decreased. The prevailing maximum velocity for a rectangular labyrinth weir at L/B = 0.61, 1.22, and 1.83 was 1.46, 1.65, and 1.84 m/s, respectively. The low mean velocities for these distances were 0.27, 0.44, and 0.72 m/s, respectively. This finding highlights the importance of weir spacing in determining the flow characteristics within the fishway.
  • The presence of an orifice in the weir increased the flow velocity at the orifice and in the middle of the pool, especially in a conventional weir. The increase ranged from 7.7 to 12.48%.
  • For a given bottom slope, in a conventional weir, the highest values of turbulent kinetic energy (TKE) are uniformly distributed in the upstream part of the weir in the cross section of the channel. In contrast, for the rectangular labyrinth weir, the highest TKE values were concentrated on the sides of the pool between the crest of the weir and the channel wall. The highest TKE value for the conventional and the rectangular labyrinth weir was 0.224 and 0.278 J/kg, respectively, at the highest bottom slope (S0 = 10%).
  • For a given discharge, bottom slope, and weir spacing, the average values of TI are higher for the rectangular labyrinth weir than for the conventional weir. At the highest discharge, the average range of turbulence intensity (TI) for the conventional and rectangular labyrinth weirs was between 24 and 45% and 15% and 62%, respectively. This reveals that the rectangular labyrinth weir may generate more turbulent flow conditions within the fishway.
  • For a given discharge and constant bottom slope, the rectangular labyrinth weir has a higher energy dissipation rate than the conventional weir (22.75 and 34.86%).
  • Increasing the distance between weirs decreased volumetric energy dissipation. However, increasing the gradient increased volumetric energy dissipation. The presence of an opening in the weir resulted in a decrease in volumetric energy dissipation for both model types.

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비선형 파력의 영향에 따른 잔해 언덕 방파제 형상의 효과에 대한 수치 분석

비선형 파력의 영향에 따른 잔해 언덕 방파제 형상의 효과에 대한 수치 분석

Numerical Analysis of the Effects of Rubble Mound Breakwater Geometry Under the Effect of Nonlinear Wave Force

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Abstract

Assessing the interaction of waves and porous offshore structures such as rubble mound breakwaters plays a critical role in designing such structures optimally. This study focused on the effect of the geometric parameters of a sloped rubble mound breakwater, including the shape of the armour, method of its arrangement, and the breakwater slope. Thus, three main design criteria, including the wave reflection coefficient (Kr), transmission coefficient (Kt), and depreciation wave energy coefficient (Kd), are discussed. Based on the results, a decrease in wavelength reduced the Kr and increased the Kt and Kd. The rubble mound breakwater with the Coreloc armour layer could exhibit the lowest Kr compared to other armour geometries. In addition, a decrease in the breakwater slope reduced the Kr and Kd by 3.4 and 1.25%, respectively. In addition, a decrease in the breakwater slope from 33 to 25° increased the wave breaking height by 6.1% on average. Further, a decrease in the breakwater slope reduced the intensity of turbulence depreciation. Finally, the armour geometry and arrangement of armour layers on the breakwater with its different slopes affect the wave behaviour and interaction between the wave and breakwater. Thus, layering on the breakwater and the correct use of the geometric shapes of the armour should be considered when designing such structures.

파도와 잔해 더미 방파제와 같은 다공성 해양 구조물의 상호 작용을 평가하는 것은 이러한 구조물을 최적으로 설계하는 데 중요한 역할을 합니다. 본 연구는 경사진 잔해 둔덕 방파제의 기하학적 매개변수의 효과에 초점을 맞추었는데, 여기에는 갑옷의 형태, 배치 방법, 방파제 경사 등이 포함된다. 따라서 파동 반사 계수(Kr), 투과 계수(Kt) 및 감가상각파 에너지 계수(Kd)에 대해 논의합니다. 결과에 따르면 파장이 감소하면 K가 감소합니다.r그리고 K를 증가시켰습니다t 및 Kd. Coreloc 장갑 층이 있는 잔해 언덕 방파제는 가장 낮은 K를 나타낼 수 있습니다.r 다른 갑옷 형상과 비교했습니다. 또한 방파제 경사가 감소하여 K가 감소했습니다.r 및 Kd 각각 3.4%, 1.25% 증가했다. 또한 방파제 경사가 33°에서 25°로 감소하여 파도 파쇄 높이가 평균 6.1% 증가했습니다. 또한, 방파제 경사의 감소는 난류 감가상각의 강도를 감소시켰다. 마지막으로, 경사가 다른 방파제의 장갑 형상과 장갑 층의 배열은 파도 거동과 파도와 방파제 사이의 상호 작용에 영향을 미칩니다. 따라서 이러한 구조를 설계 할 때 방파제에 층을 쌓고 갑옷의 기하학적 모양을 올바르게 사용하는 것을 고려해야합니다.

Keywords

  • Rubble mound breakwater
  • Computational fluid dynamics
  • Armour layer
  • Wave reflection coefficient
  • Wave transmission coefficient
  • Wave energy dissipation coefficient

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Open Channels Flow에서의 콘크리트 캔버스 거동 연구

Study of Concrete Canvas Behavior in Open Channels Flow

Document Type : Research Paper

Authors

1 Imam Hosein Uni

2 Researcher of Imam Hossein University, Faculty of Engineering and Passive Defense

3 Ivanki University, Iran.

 10.22124/JCR.2023.24324.1618

Abstract

개방 수로의 심한 수력 구배는 침전으로 인한 심각한 침식과 문제를 일으킵니다. 패브릭 콘크리트는 기존의 콘크리트 표면을 대체할 수 있는 높은 실행 속도를 가진 독특한 제품입니다. 이 제품의 기계적 저항 매개변수에 따르면 부식 요인에 대한 우수한 내구성 외에도 직물 콘크리트의 응용 분야 중 하나는 운하 및 수로 암거 표면에 사용하는 것입니다. 이 연구에서는 먼저 사다리꼴 단면의 개방 채널 흐름을 직선 경로 상태의 3가지 공통 채널 형상, 굴곡 및 편차가 있는 경로, 마지막으로 채널 하단의 높이가 변경된 채널 경로를 포함하는 9가지 시나리오에서 시뮬레이션합니다. 각 주에서 flow-3d 소프트웨어를 사용한 흐름 난류 모델링과 함께 3개의 서로 다른 흐름 체제가 조사되었습니다.

FLOW-3D 소프트웨어를 사용한 유동 난류 모델링과 함께 다양한 유동 체제가 조사되었습니다. ABAQUS 소프트웨어를 사용하여 패브릭 콘크리트 구성요소와 연결 영역을 모델링하고, 콘크리트 표면과 취약한 연결 영역에 동일한 힘을 가하여 생성된 응력의 양을 확인했습니다. 결과는 생성된 응력이 직물 콘크리트의 인장 및 압축 응력 용량에 비해 매우 낮다는 것을 보여줍니다. 흐름과 콘크리트의 수력 연구를 검증하기 위해 관련 실험실 결과가 사용되었습니다.

Severe hydraulic gradients in open channels cause severe bed erosion and problems caused by sedimentation. Fabric concrete is a unique product with high execution speed that can replace traditional concrete surfaces. According to the mechanical resistance parameters of this product, in addition to its good durability against corrosive factors, one of the applications of fabric concrete is its use on the surface of canals and water course culverts. In this research, first, the flow of open channels in trapezoidal section is simulated under 9 scenarios, which include 3 common channel geometries in the state of a straight path, a path with bends and deviations, and finally, a channel path with a change in height at the bottom of the channel. In each of the states, 3 different flow regimes have been investigated along with flow turbulence modeling using flow-3d software.

Different flow regimes have been investigated along with flow turbulence modeling using flow-3d software. Using ABAQUS software, fabric concrete components and their connection areas have been modeled, and by applying forces equated to the concrete surface and vulnerable connection areas, the amount of created stresses has been checked. The results show that the created stresses are very low compared to the tensile and compressive stress capacity of fabric concrete. In order to validate the hydraulic studies of flow and concrete, the relevant laboratory results have been used.

Keywords

Main Subjects

Study on the critical sediment concentration determining the optimal transport capability of submarine sediment flows with different particle size composition

Study on the critical sediment concentration determining the optimal transport capability of submarine sediment flows with different particle size composition

Yupeng Ren abc, Huiguang Zhou cd, Houjie Wang ab, Xiao Wu ab, Guohui Xu cd, Qingsheng Meng cd

Abstract

해저 퇴적물 흐름은 퇴적물을 심해로 운반하는 주요 수단 중 하나이며, 종종 장거리를 이동하고 수십 또는 수백 킬로미터에 걸쳐 상당한 양의 퇴적물을 운반합니다. 그것의 강력한 파괴력은 종종 이동 과정에서 잠수함 유틸리티에 심각한 손상을 초래합니다.

퇴적물 흐름의 퇴적물 농도는 주변 해수와의 밀도차를 결정하며, 이 밀도 차이는 퇴적물 흐름의 흐름 능력을 결정하여 이송된 퇴적물의 최종 퇴적 위치에 영향을 미칩니다. 본 논문에서는 다양한 미사 및 점토 중량비(미사/점토 비율이라고 함)를 갖는 다양한 퇴적물 농도의 퇴적물 흐름을 수로 테스트를 통해 연구합니다.

우리의 테스트 결과는 특정 퇴적물 구성에 대해 퇴적물 흐름이 가장 빠르게 이동하는 임계 퇴적물 농도가 있음을 나타냅니다. 4가지 미사/점토 비율 각각에 대한 임계 퇴적물 농도와 이에 상응하는 최대 속도가 구해집니다. 결과는 점토 함량이 임계 퇴적물 농도와 선형적으로 음의 상관 관계가 있음을 나타냅니다.

퇴적물 농도가 증가함에 따라 퇴적물의 흐름 거동은 흐름 상태에서 붕괴된 상태로 변환되고 흐름 거동이 변화하는 두 탁한 현탁액의 유체 특성은 모두 Bingham 유체입니다.

또한 본 논문에서는 퇴적물 흐름 내 입자 배열을 분석하여 위에서 언급한 결과에 대한 미시적 설명도 제공합니다.

Submarine sediment flows is one of the main means for transporting sediment to the deep sea, often traveling long-distance and transporting significant volumes of sediment for tens or even hundreds of kilometers. Its strong destructive force often causes serious damage to submarine utilities on its course of movement. The sediment concentration of the sediment flow determines its density difference with the ambient seawater, and this density difference determines the flow ability of the sediment flow, and thus affects the final deposition locations of the transported sediment. In this paper, sediment flows of different sediment concentration with various silt and clay weight ratios (referred to as silt/clay ratio) are studied using flume tests. Our test results indicate that there is a critical sediment concentration at which sediment flows travel the fastest for a specific sediment composition. The critical sediment concentrations and their corresponding maximum velocities for each of the four silt/clay ratios are obtained. The results further indicate that the clay content is linearly negatively correlated with the critical sediment concentration. As the sediment concentration increases, the flow behaviors of sediment flows transform from the flow state to the collapsed state, and the fluid properties of the two turbid suspensions with changing flow behaviors are both Bingham fluids. Additionally, this paper also provides a microscopic explanation of the above-mentioned results by analyzing the arrangement of particles within the sediment flow.

Introduction

Submarine sediment flows are important carriers for sea floor sediment movement and may carry and transport significant volumes of sediment for tens or even hundreds of kilometers (Prior et al., 1987; Pirmez and Imran, 2003; Zhang et al., 2018). Earthquakes, storms, and floods may all trigger submarine sediment flow events (Hsu et al., 2008; Piper and Normark, 2009; Pope et al., 2017b; Gavey et al., 2017). Sediment flows have strong forces during the movement, which will cause great harm to submarine structures such as cables and pipelines (Pope et al., 2017a). It was first confirmed that the cable breaking event caused by the sediment flow occurred in 1929. The sediment flow triggered by the Grand Banks earthquake damaged 12 cables. According to the time sequence of the cable breaking, the maximum velocity of the sediment flow is as high as 28 m/s (Heezen and Ewing, 1952; Kuenen, 1952; Heezen et al., 1954). Subsequent research shows that the lowest turbidity velocity that can break the cable also needs to reach 19 m/s (Piper et al., 1988). Since then, there have been many damage events of submarine cables and oil and gas pipelines caused by sediment flows in the world (Hsu et al., 2008; Carter et al., 2012; Cattaneo et al., 2012; Carter et al., 2014). During its movement, the sediment flow will gradually deposit a large amount of sediment carried by it along the way, that is, the deposition process of the sediment flow. On the one hand, this process brings a large amount of terrestrial nutrients and other materials to the ocean, while on the other hand, it causes damage and burial to benthic organisms, thus forming the largest sedimentary accumulation on Earth – submarine fans, which are highly likely to become good reservoirs for oil and gas resources (Daly, 1936; Yuan et al., 2010; Wu et al., 2022). The study on sediment flows (such as, the study of flow velocity and the forces acting on seabed structures) can provide important references for the safe design of seabed structures, the protection of submarine ecosystems, and exploration of turbidity sediments related oil and gas deposits. Therefore, it is of great significance to study the movement of sediment flows.

The sediment flow, as a highly sediment-concentrated fluid flowing on the sea floor, has a dense bottom layer and a dilute turbulent cloud. Observations at the Monterey Canyon indicated that the sediment flow can maintain its movement over long distances if its bottom has a relatively high sediment concentration. This dense bottom layer can be very destructive along its movement path to any facilities on the sea floor (Paull et al., 2018; Heerema et al., 2020; Wang et al., 2020). The sediment flow mentioned in this research paper is the general term of sediment density flow.

The sediment flow, which occurs on the seafloor, has the potential to cause erosion along its path. In this process, the suspended sediment is replenished, allowing the sediment flow to maintain its continuous flow capacity (Zhao et al., 2018). The dynamic force of sediment flow movement stem from its own gravity and density difference with surrounding water. In cases that the gravity drive of the slope is absent (on a flat sea floor), the flow velocity and distance of sediment flows are essentially determined by the sediment composition and concentration of the sediment flows as previous studies have demonstrated. Ilstad et al. (2004) conducted underwater flow tests in a sloped tank and employed high speed video camera to perform particle tracking. The results indicated that the premixed sand-rich and clay-rich slurries demonstrated different flow velocity and flow behavior. Using mixed kaolinite(d50 = 6 μm) and silica flour(d50 = 9 μm) in three compositions with total volumetric concentration ranged 22% or 28%, Felix and Peakall (2006) carried out underwater flow tests in a 5° slope Perspex channel and found that the flow ability of sediment flows is different depending on sediment compositions and concentrations. Sumner et al. (2009) used annular flume experiments to investigate the depositional dynamics and deposits of waning sediment-laden flows, finding that decelerating fast flows with fixed sand content and variable mud content resulted in four different deposit types. Chowdhury and Testik (2011) used lock-exchange tank, and experimented the kaolin clay sediment flows in the concentration range of 25–350 g/L, and predicted the fluid mud sediment flows propagation characteristics, but this study focused on giving sediment flows propagate phase transition time parameters, and is limited to clay. Lv et al. (2017) found through experiments that the rheological properties and flow behavior of kaolin clay (d50 = 3.7 μm) sediment flows were correlated to clay concentrations. In the field monitoring conducted by Liu et al. (2023) at the Manila Trench in the South China Sea in 2021, significant differences in the velocity, movement distance, and flow morphology of turbidity currents were observed. These differences may be attributed to variations in the particle composition of the turbidity currents.

On low and gentle slopes, although sediment flow with sand as the main sediment composition moves faster, it is difficult to propagate over long distances because sand has greater settling velocity and subaqueous angle of repose. Whereas the sediment flows with silt and clay as main composition may maintain relatively stable currents. Although its movement speed is slow, it has the ability to propagate over long distances because of the low settling rate of the fine particles (Ilstad et al., 2004; Liu et al., 2023). In a field observation at the Gaoping submarine canyon, the sediments collected from the sediment flows exhibited grain size gradation and the sediment was mostly composed of silt and clay (Liu et al., 2012). At the largest deltas in the world, for instance, the Mississippi River Delta, the sediments are mainly composed of silt and clay, which generally distributed along the coast in a wide range and provided the sediment sources for further distribution. The sediment flows originated and transported sediment from the coast to the deep sea are therefore share the same sediment compositions as delta sediments. To study the sediment flows composed of silt and clay is of great importance.

The sediment concentration of the sediment flows determines the density difference between the sediment flows and the ambient water and plays a key role in its flow ability. For the sediment flow with sediment composed of silt and clay, low sediment concentration means low density and therefore leads to low flow ability; however, although high sediment concentration results in high density, since there is cohesion between fine particles, it changes fluid properties and leads to low flow ability as well. Therefore, there should be a critical sediment concentration with mixed composition of silt and clay, at which the sediment flow maintains its strongest flow capacity and have the highest movement speed. In other words, the two characteristics of particle diameter and concentration of the sediment flow determine its own motion ability, which, if occurs, may become the most destructive force to submarine structures.

The objectives of this work was to study how the sediment composition (measured in relative weight of silt and clay, and referred as silt/clay ratio) and sediment concentration affect flow ability and behavior of the sediment flows, and to quantify the critical sediment concentration at which the sediment flows reached the greatest flow velocity under the experiment setting. We used straight flume without slope and conducted a series of flume tests with varying sediment compositions (silt-rich or clay-rich) and concentrations (96 to 1212 g/L). Each sediment flow sample was tested and analyzed for rheological properties using a rheometer, in order to characterize the relationship between flow behavior and rheological properties. Combined with the particle diameter, density and viscosity characteristics of the sediment flows measured in the experiment, a numerical modeling study is conducted, which are mutually validated with the experimental results.

The sediment concentration determines the arrangements of the sediment particles in the turbid suspension, and the arrangement impacts the fluid properties of the turbid suspension. The microscopic mode of particle arrangement in the turbid suspension can be constructed to further analyze the relationship between the fluid properties of turbid suspension and the flow behaviors of the sediment flow, and then characterize the critical sediment concentration at which the sediment flow runs the fastest. A simplified microscopic model of particle arrangement in turbid suspension was constructed to analyze the microscopic arrangement characteristics of sediment particles in turbid suspension with the fastest velocity.

Section snippets

Equipment and materials

The sediment flows flow experiments were performed in a Perspex channel with smooth transparent walls. The layout and dimensions of the experimental set-up were shown in Fig. 1. The bottom of the channel was flat and straight, and a gate was arranged to separate the two tanks. In order to study the flow capacity of turbidity currents from the perspective of their own composition (particle size distribution and concentration), we used a straight channel instead of an inclined one, to avoid any

Relationship between sediment flow flow velocity and sediment concentration

After the sediment flow is generated, its movement in the first half (50 cm) of the channel is relatively stable, and there is obvious shock diffusion in the second half. The reason is that the excitation wave (similar to the surge) will be formed during the sediment flow movement, and its speed is much faster than the speed of the sediment flow head. When the excitation wave reaches the tail of the channel, it will be reflected, thus affecting the subsequent flow of the sediment flow.

Sediment flows motion simulation based on FLOW-3D

As a relatively mature 3D fluid simulation software, FLOW-3D can accurately predict the free surface flow, and has been used to simulate the movement process of sediment flows for many times (Heimsund, 2007). The model adopted in this paper is RNG turbulence model, which can better deal with the flow with high strain rate and is suitable for the simulation of sediment flows with variable shape during movement. The governing equations of the numerical model involved include continuity equation,

Conclusions

In this study, we conducted a series of sediment flow flume tests with mixed silt and clay sediment samples in four silt/clay ratios on a flat slope. Rheological measurements were carried out on turbid suspension samples and microstructure analysis of the sediment particle arrangements was conducted, we concluded that:

  • (1)The flow velocity of the sediment flow is controlled by the sediment concentration and its own particle diameter composition, the flow velocity increased with the increase of the

Declaration of Competing Interest

The authors declare that they have no known competing financial interests or personal relationships that could have appeared to influence the work reported in this paper.

Acknowledgements

This work was supported by the National Natural Science Foundation of China [Grant no. 42206055]; the National Natural Science Foundation of China [Grant no. 41976049]; and the National Natural Science Foundation of China [Grant no. 42272327].

References (39)

There are more references available in the full text version of this article.

Figure 1. Three-dimensional finite element model of local scouring of semi-exposed submarine cable.

반노출 해저케이블의 국부 정련과정 및 영향인자에 대한 수치적 연구

Numerical Study of the Local Scouring Process and Influencing Factors of Semi-Exposed Submarine Cables

by Qishun Li,Yanpeng Hao *,Peng Zhang,Haotian Tan,Wanxing Tian,Linhao Chen andLin Yang

School of Electric Power Engineering, South China University of Technology, Guangzhou 510640, China

*Author to whom correspondence should be addressed.J. Mar. Sci. Eng.202311(7), 1349; https://doi.org/10.3390/jmse11071349

Received: 10 June 2023 / Revised: 19 June 2023 / Accepted: 27 June 2023 / Published: 1 July 2023(This article belongs to the Section Ocean Engineering)

일부 수식이 손상되어 표시될 수 있습니다. 이 경우 원문을 참조하시기 바랍니다.

Abstract

Local scouring might result in the spanning of submarine cables, endangering their mechanical and electrical properties. In this contribution, a three-dimensional computational fluid dynamics simulation model is developed using FLOW-3D, and the scouring process of semi-exposed submarine cables is investigated. The effects of the sediment critical Shields number, sediment density, and ocean current velocity on local scouring are discussed, and variation rules for the submarine cables’ spanning time are provided. The results indicate that three scouring holes are formed around the submarine cables. The location of the bottom of the holes corresponds to that of the maximum shear velocity. The continuous development of scouring holes at the wake position leads to the spanning of the submarine cables. The increase in the sediment’s critical Shields number and sediment density, as well as the decrease in the ocean current velocity, will extend the time for maintaining the stability of the upstream scouring hole and retard the development velocity of the wake position and downstream scouring holes. The spanning time has a cubic relationship with the sediment’s critical Shields number, a linear relationship with the sediment density, and an exponential relationship with the ocean current velocity. In this paper, the local scouring process of semi-exposed submarine cables is studied, which provides a theoretical basis for the operation and maintenance of submarine cables.

Keywords: 

submarine cablelocal scouringnumerical simulationcomputational fluid dynamics

1. Introduction

As a key piece of equipment in cross-sea power grids, submarine cables are widely used to connect autonomous power grids, supply power to islands or offshore platforms, and transmit electric power generated by marine renewable energy installations to onshore substations [1]. Once submarine cables break down due to natural disasters or human-made damage, the normal operation of other marine electric power equipment connected to them may be affected. These chain reactions will cause great economic losses and serious social impacts [2].

To protect submarine cables, they are usually buried 1 to 3 m below the seabed [3]. However, submarine cables are still confronted with potential threats from the complex subsea environment. Under the influence of fishing, anchor damage, ocean current scouring, and other factors, the sediment above submarine cables will always inevitably migrate. When a submarine cable is partially exposed, the scouring at this position will be exacerbated; eventually, it will cause the submarine cable to span. According to a field investigation of the 500 kV oil-filled submarine cable that is part of the Hainan networking system, the total length of the span is 49 m [4]. Under strong ocean currents, spanning submarine cables may experience vortex-induced vibrations. Fatigue stress caused by vortex-induced vibrations may lead to metal sheath rupture [5], which endangers the mechanical and electrical properties of submarine cables. Therefore, understanding the local scouring processes of partially exposed submarine cables is crucial for predicting scouring patterns. This is the basis for developing effective operation and maintenance strategies for submarine cables.

The mechanism and influencing factors of sediment erosion have been examined by researchers around the world. In 1988, Sumer [6] conducted experiments to show that the shedding vortex in the wake of a pipeline would increase the Shields parameter by 3–4 times, which would result in severe scouring. In 1991, Chiew [7] performed experiments to prove that the maximum scouring depth could be obtained when the pipeline was located on a flat bed and was scoured by a unidirectional water flow. Based on the test results, they provided a prediction formula for the maximum scouring depth. In 2003, Mastbergen [8] proposed a one-dimensional, steady-state numerical model of turbidity currents, which considered the negative pore pressures in the seabed. The calculated results of this model were basically consistent with the actual scouring of a submarine canyon. In 2007, Dey [9] presented a semitheoretical model for the computation of the maximum clear-water scour depth below underwater pipelines in uniform sediments under a steady flow, and the predicted scour depth in clear water satisfactorily agreed with the observed values. In 2008, Dey [10] conducted experiments on clear-water scour below underwater pipelines under a steady flow and obtained a variation pattern of the depth of the scouring hole. In 2008, Liang [11] used a two-dimensional numerical simulation to study the scouring process of a tube bundle under the action of currents and waves. They discovered that, compared with the scouring of a single tube, the scouring depth of the tube bundle was deeper, and the scouring time was longer. In 2012, Yang [12] found that placing rubber sheets under pipes can greatly accelerate their self-burial. The rubber sheets had the best performance when their length was about 1.5 times the size of the pipe. In 2020, Li [13] investigated the two-dimensional local scour beneath two submarine pipelines in tandem under wave-plus-current conditions via numerical simulation. They found that for conditions involving waves plus a low-strength current, the scour pattern beneath the two pipelines behaved like that in the pure-wave condition. Conversely, when the current had equal strength to the wave-induced flow, the scour pattern beneath the two pipelines resembled that in the pure-current condition. In 2020, Guan [14] studied and discussed the interactive coupling effects among a vibrating pipeline, flow field, and scour process through experiments, and the experimental data showed that the evolution of the scour hole had significant influences on the pipeline vibrations. In 2021, Liu [15] developed a two-dimensional finite element numerical model and researched the local scour around a vibrating pipeline. The numerical results showed that the maximum vibration amplitude of the pipeline could reach about 1.2 times diameter, and the maximum scour depth occurred on the wake side of the vibrating pipeline. In 2021, Huang [16] carried out two-dimensional numerical simulations to investigate the scour beneath a single pipeline and piggyback pipelines subjected to an oscillatory flow condition at a KC number of 11 and captured typical steady-streaming structures around the pipelines due to the oscillatory flow condition. In 2021, Cui [17] investigated the characteristics of the riverbed scour profile for a pipeline buried at different depths under the condition of riverbed sediments with different particle sizes. The results indicated that, in general, the equilibrium scour depth changed in a spoon shape with the gradual increase in the embedment ratio. In 2022, Li [18] used numerical simulation to study the influence of the burial depth of partially buried pipelines on the surrounding flow field, but they did not investigate the scour depth. In 2022, Zhu [19] performed experiments to prove that the scour hole propagation rate under a pipeline decreases with an increasing pipeline embedment ratio and rises with the KC number. In 2022, Najafzadeh [20] proposed equations for the prediction of the scouring propagation rate around pipelines due to currents based on a machine learning model, and the prediction results were consistent with the experimental data. In 2023, Ma [21] used the computational fluid dynamics coarse-grained discrete element method to simulate the scour process around a pipeline. The results showed that this method can effectively reduce the considerable need for computing resources and excessive computation time. In 2023, through numerical simulations, Hu [22] discovered that the water velocity and the pipeline diameter had a significant effect on the depth of scouring.

In the preceding works, the researchers investigated the mechanism of sediment scouring and the effect of various factors on the local scouring of submarine pipelines. However, submarine cables are buried beneath the seabed, while submarine pipelines are erected above the seabed. The difference in laying methods leads to a large discrepancy between their local scouring processes. Therefore, the conclusions of the above investigations are not applicable to the local scouring of submarine cables. Currently, there is no report on the research of the local scouring of partially exposed submarine cables.

In this paper, a three-dimensional computational fluid dynamics (CFD) finite element model, based on two-phase flow, is established using FLOW-3D. The local scouring process of semi-exposed submarine cables under steady-state ocean currents is studied, and the variation rules of the depth and the shape of the scouring holes, as well as the shear velocity with time, are obtained. By setting different critical Shields numbers of the sediment, different sediment densities, and different ocean current velocities, the change rule of the scouring holes’ development rate and the time required for the spanning of submarine cables are explored.

2. Sediment Scouring Model

In the sediment scouring model, the sediment is set as the dispersed particle, which is regarded as a kind of quasifluid. In this context, sediment scouring is considered as a two-phase flow process between the liquid phase and solid particle phase. The sediment in this process is further divided into two categories: one is suspended in the fluid, and the other is deposited on the bottom.When the local Shields number of sediment is greater than the critical Shields number, the deposited sediment will be transformed into the suspended sediment under the action of ocean currents. The calculation formulae of the local Shields numbers θ and the critical Shields numbers 

θcr of sediment is given as [23,24

]

𝜃=𝑈2𝑓(𝜌𝑠/𝜌𝑓−1)𝑔𝑑50,�=��2(��/��−1)��50,(1)

𝜃𝑐𝑟=0.31+1.2𝐷∗+0.055(1−𝑒−0.02𝐷∗),���=0.31+1.2�*+0.055(1−�−0.02�*),(2)

𝐷∗=𝑑50𝜌𝑓(𝜌𝑠−𝜌𝑓)𝑔/𝜇2−−−−−−−−−−−−−−√3,�*=�50��(��−��)�/�23,(3)where 

Uf is the shearing velocity of bed surface, 

ρs is the density of the sediment particle, 

ρf is the fluid density, g is the acceleration of gravity, d

50 is the median size of sediment, and μ is the dynamic viscosity of sediment.And each sediment particle suspended in the fluid obeys the equations for mass conservation and energy conservation

∂𝑐𝑠∂𝑡+∇⋅(𝑢𝑐𝑠)=0,∂��∂�+∇⋅(�¯��)=0,(4)

∂𝑢𝑠∂𝑡+𝑢⋅∇𝑢𝑠=−1𝜌𝑠∇𝑃+𝐹−𝐾𝑓𝑠𝜌𝑠𝑢𝑟,∂��∂�+�¯⋅∇��=−1��∇�+�−�������,(5)where 

cs is the concentration of the sediment particle, 

𝑢�¯ is the mean velocity vector of the fluid and the sediment particle, 

us is the velocity of the sediment particle, 

fs is the volume fraction of the sediment particle, P is the pressure, F is the volumetric and viscous force, K is the drag force, and 

ur is the relative velocity.

3. Numerical Setup and Modeling

In this paper, a three-dimensional submarine cable local scouring simulation model is established by FLOW-3D. Based on the numerical simulation, the process of the submarine cable, which gradually changes from semi-exposed to the spanning state under the steady-state ocean current, is studied. The geometric modeling, the mesh division, the physical field setup, and the grid independent test of CFD numerical model are as follows.

3.1. Geometric Modeling and Mesh Division

A three-dimensional (3D) numerical model of the local scouring of a semi-exposed submarine cable is established, which is shown in Figure 1. The dimensions of the model are marked in Figure 1. The inlet direction of the ocean current is defined as the upstream of the submarine cable (referred to as upstream), and the outlet direction of the ocean current is defined as the downstream of the submarine cable (referred to as downstream).

Jmse 11 01349 g001 550

Figure 1. Three-dimensional finite element model of local scouring of semi-exposed submarine cable.

The submarine cable with a diameter of 0.2 m is positioned on sediment that is initially in a semi-exposed state. When the length of the span is short, the submarine cable will not show obvious deformation due to gravity or scouring from the ocean current. Therefore, the submarine cable surface is set as the fixed boundary. The model’s left boundary is set as the inlet, the right boundary is set as the outlet, the front and rear boundaries are set as symmetry, and the bottom boundary is set as the non-slip wall. Since the water depth above the submarine cable is more than 0.6 m in practice, the top boundary of the model is also set as symmetry. The sediment near the inlet and the outlet will be carried by ocean currents, which leads to the abnormal scouring terrain. At each end of the sediment, a baffle (thickness of 3 cm) is installed to ensure that the simulation results can reflect the real situation.

Due to the fact that the flow field around the semi-exposed submarine cable is not a simple two-dimensional symmetrical distribution, it should be solved by three-dimensional numerical simulation. Considering the accuracy and efficiency of the calculation, the size of mesh is set to 0.02 m. The total number of meshes after the dissection is 133,254.

3.2. Physical Field Setup

The CFD finite element model contains four physical field modules: sediment scouring module, gravity and non-inertial reference frame module, density evaluation module, and viscosity and turbulence module. In this paper, the renormalization group (RNG) kε turbulence model is used, which has high computational accuracy for turbulent vortices. Therefore, this turbulence model is suitable for calculating the sediment scouring process around the semi-exposed submarine cable [25]. The key parameters of the numerical simulation are referring to the survey results of submarine sediments in the Korean Peninsula [26], as listed in Table 1.Table 1. Key parameters of numerical simulation.

Table

3.3. Mesh Independent Test

In order to eliminate errors caused by the quantity of grids in the calculation process, two sizes of mesh are set on the validation model, and the scour profiles under different mesh sizes are compared. The validation model is shown in Figure 2, and the scouring terrain under different mesh size is given in Figure 3.

Jmse 11 01349 g002 550

Figure 2. Validation model.

Jmse 11 01349 g003 550

Figure 3. Scouring terrain under different mesh sizes.

It can be seen from Figure 3 that with the increase in the number of meshes, the scouring terrain of the verification model changes slightly, and the scouring depth is basically unchanged. Considering the accuracy of the numerical simulation and the calculation’s time cost, it is reasonable to consider setting the mesh size to 0.02 m.

4. Results and Analysis

4.1. Analysis of Local Scouring Process

Based on the CFD finite element numerical simulation, the local scouring process of the submarine cable under the steady-state ocean current is analyzed. The end time of the simulation is 9 h, the initial time step is 0.01 s, and the fluid velocity is 0.40 m/s. Simulation results are saved every minute. Figure 4 illustrates the scouring terrain around the semi-exposed submarine cable, which has been scoured by the steady-state current for 5 h.

Jmse 11 01349 g004 550

Figure 4. Scouring terrain around semi-exposed submarine cable (scour for 5 h).

As can be seen from Figure 4, three scouring holes were separately formed in the upstream wake position and downstream of the semi-exposed submarine cable. The scouring holes are labeled according to their locations. The variation of the scouring terrain around the semi-exposed submarine cable over time is given in Figure 5. The red circle in the picture corresponds to the position of the submarine cable, and the red box in the legend marks the time when the submarine cable is spanning.

Jmse 11 01349 g005 550

Figure 5. Variation of scouring terrain around semi-exposed submarine cable adapted to time.

From Figure 5, in the first hour of scouring, the upstream (−0.5 m to −0.1 m) and downstream (0.43 m to 1.5 m) scouring holes appeared. The upstream scouring hole was relatively flat with depth of 0.04 m. The depth of the downstream scouring hole increased with the increase in distance, and the maximum depth was 0.13 m. The scouring hole that developed at the wake position was very shallow, and its depth was only 0.007 m.

In the second hour of scouring, the upstream scouring hole’s depth remained nearly constant. The depth of the downstream scouring hole only increased by 0.002 m. The scouring hole at the wake position developed steadily, and its depth increased from 0.007 m to 0.014 m.

The upstream and downstream scouring holes did not continue to develop during the third to the sixth hour. Compared to the first two hours, the development of scouring holes at the wake position accelerated significantly, with an average growth rate of 0.028 m/h. The growth rate in the fifth hour of the scouring hole at the wake position was slightly faster than the other times. After 6 h of scouring, the sediment on the right side of the submarine cable had been hollowed out.

In the seventh and the eighth hour of scouring, the upstream scouring hole’s depth increased slightly, the downstream scouring hole still remained stable, and the depth of the scouring hole at wake position increased by 0.019 m. The sediment under the submarine cable was gradually eroded as well. By the end of the eighth hour, the lower right part of the submarine cable had been exposed to water as well.

At 8 h 21 min of the scouring, the submarine cable was completely spanned, and the scouring holes were connected to each other. Within the next 10 min, the development of the scouring holes sped up significantly, and the maximum depth of scouring holes increased greatly to 0.27 m.

In reference [17], researchers have studied the local scouring process of semi-buried pipelines in sandy riverbeds through experiments. The test results show that the scouring process can be divided into a start-up stage, micropore formation stage, extension stage, and equilibrium stage. In this paper, the first three stages are simulated, and the results are in good agreement with the experiment, which proves the accuracy of the present numerical model.

In this research, the velocity of ocean currents at the sediment surface is defined as the shear velocity, which plays an important role in the process of local scouring. Figure 6 provides visual data on how the shear velocity varies over time.

Jmse 11 01349 g006 550

Figure 6. Shear velocity changes in the scouring process.

The semi-exposed submarine cable protrudes from the seabed, which makes the shear velocity of its surface much higher than other locations. After the submarine cable is spanned, the shear velocity of the scouring hole surface below it is taken. This is the reason for the sudden change of shear velocity at the submarine cable’s location in Figure 6.The shear velocity in the initial state of the upstream scouring hole is obviously greater than in subsequent times. After 1 h of scouring, the shear velocity in the upstream scouring hole rapidly decreased from 1.1 × 10

−2 m/s to 3.98 × 10

−3 m/s and remained stable until the end of the sixth hour. This phenomenon explains why the upstream scouring hole developed rapidly in the first hour but remained stable for the following 5 h.The shear velocity in the downstream scouring hole reduced at first and then increased; its initial value was 1.41 × 10

−2 m/s. It took approximately 5 h for the shear velocity to stabilize, and the stable shear velocity was 2.26 × 10

−3 m/s. Therefore, compared with the upstream scouring hole, the downstream scouring hole was deeper and required more time to reach stability.The initial shear velocity in the scouring hole at the wake position was only 7.1 × 10

−3 m/s, which almost does not change in the first hour. This leads to a very slow development of the scouring hole at the wake position in the early stages. The maximum shear velocity in this scouring hole gradually increased to 1.05 × 10

−2 m/s from the second to the fifth hour, and then decreased to 6.61 × 10

−3 m/s by the end of the eighth hour. This is why the scouring hole at the wake position grows fastest around the fifth hour. Consistent with the pattern of change in the scouring hole’s terrain, the location of the maximal shear velocity also shifted to the right with time.

The shear velocity of all three scouring holes rose dramatically in the last hour. Combined with the terrain in Figure 5, this can be attributed to the complete spanning of the submarine cable.

From Equations (3)–(5), one can see the movement of the sediment is related directly with the sediment’s critical Shields number, sediment density, and ocean current velocity. Based on the parameters in Table 1, the influence of the above parameters on the local scouring process of semi-exposed submarine cables will be discussed.

4.2. Influence Factors

4.2.1. Sediment’s Critical Shields Number

The sediment’s critical Shields number 

θcr is set as 0.02, 0.03, 0.04, 0.05, 0.06, and 0.07, and the variations of scouring terrain over time under each 

θcr are displayed in Figure 7.

Jmse 11 01349 g007 550

Figure 7. Influence of sediment’s critical Shields number 

θcr on local scouring around semi-exposed submarine cable: (a

θcr = 0.02; (b

θcr = 0.03; (c

θcr = 0.04; (d

θcr = 0.05; (e

θcr = 0.06; and (f

θcr = 0.07.From Figure 7, one can see that a change in 

θcr will affect the depth of the upstream scouring hole and the development speed of the scouring hole at the wake position, but it will have no significant impact on the expansion of the downstream scouring hole.Under conditions of different 

θcr, the upstream scouring hole will reach a temporary plateau within 1 h, at which time the stable depth will be about 0.04 m. When 

θcr ≤ 0.05, the upstream scouring hole will continue to expand after a few hours. The stable time is obviously affected by 

θcr, which will gradually increase from 1 h to 11 h with the increase in 

θcr. The terrain of the upstream scouring hole will gradually convert to deep on the left and to shallow on the right. Since the scouring hole at the wake position has not been stable, its state at the time of submarine cable spanning is studied emphatically. In the whole process of scouring, the scouring hole at the wake position continues to develop and does not reach a stable state. With the increase in 

θcr, the development velocity of the scouring hole at the wake position will decrease considerably. Its average evolution velocity decreases from 3.88 cm/h to 1.62 cm/h, and its depth decreases from 21.9 cm to 18.8 cm. Under the condition of each 

θcr, the downstream scouring hole will stabilize within 1 h, and the stable depth will be basically unchanged (all about 13.5 cm).As 

θcr increases, so does the sediment’s ability to withstand shearing forces, which will cause it to become increasingly difficult to be eroded or carried away by ocean currents. This effect has been directly reflected in the depth of scouring holes (upstream and wake position). Due to the blocking effect of semi-exposed submarine cables, the wake is elongated, which is why the downstream scouring hole develops before the scouring hole at the wake position and quickly reaches a stable state. However, due to the high wake intensity, this process is not significantly affected by the change of 

θcr.

4.2.2. Sediment Density

The density of sediment 

ρs is set as 1550 kg/m

3, 1600 kg/m

3, 1650 kg/m

3, 1700 kg/m

3, 1750 kg/m

3, and 1800 kg/m

3, and the variation of scouring terrain over time under each 

ρs are displayed in Figure 8.

Jmse 11 01349 g008 550

Figure 8. Influence of sediment density 

ρs on local scouring around semi-exposed submarine cable: (a

ρs = 1550 kg/m

3; (bρs = 1600 kg/m

3; (cρs = 1650 kg/m

3; (dρs = 1700 kg/m

3; (eρs = 1750 kg/m

3; and (f

ρs = 1800 kg/m

3.From Figure 8, one can see that a change in 

ρs will also affect the depth of the upstream scouring hole and the development speed of the scouring hole at the wake position. In addition, it can even have an impact on the downstream scouring hole depth.Under different 

ρs conditions, the upstream scouring hole will always reach a temporary stable state in 1 h, at which time the stable depth will be 0.04 m. When 

ρs ≤ 1750 kg/m

3, the upstream scouring hole will continue to expand after a few hours. The stabilization time of upstream scouring hole is more clearly affected by 

ρs, which will gradually increase from 3 h to 13 h with the increase in 

ρs. The terrain of the upstream scouring hole will gradually change to deep on the left and to shallow on the right. Since the scouring hole at the wake position has not been stable, its state at the time of the submarine cable spanning is studied emphatically, too. In the whole process of scouring, the scouring hole at the wake position continues to develop and does not reach a stable state. When 

ρs is large, the development rate of scouring hole obviously decreased with time. With the increase in 

ρs, the development velocity of the scouring hole at the wake position reduces from 3.38 cm/h to 1.14 cm/h, and the depth of this scouring hole declines from 20 cm to 15 cm. As 

ρs increases, the stabilization time of the downstream scouring hole increases from less than 1 h to about 2 h, but the stabilization depth of the downstream scouring hole remains essentially the same (all around 13.5 cm).As can be seen from Equation (1), the increase in 

ρs will reduce the Shields number, thus weakening the shear action of the sediment by the ocean current, which explains the extension of the stability time of the upstream scouring hole. At the same time, with the increase in the depth of scouring hole at the wake position, its shear velocity will decreases. Therefore, under a larger 

ρs value, the development speed of scouring hole at the wake position will decrease significantly with time. Possibly for the same reason, 

ρs can affect the development rate of downstream scouring hole.

4.2.3. Ocean Current Velocity

The ocean current velocity v is set as 0.35 m/s, 0.40 m/s, 0.45 m/s, 0.50 m/s, 0.55 m/s, and 0.60 m/s. Figure 9 presents the variation in scouring terrain with time for each v.

Jmse 11 01349 g009 550

Figure 9. Influence of ocean current velocity v on local scouring around semi-exposed submarine cable: (av = 0.35 m/s; (bv = 0.40 m/s; (cv = 0.45 m/s; (dv = 0.50 m/s; (ev = 0.55 m/s; and (fv = 0.60 m/s.

Changes in v affect the depth of the upstream and downstream scouring holes, as well as the development velocity of the wake position and downstream scouring holes.

When v ≤ 0.45 m/s, the upstream scouring hole will reach a temporary stable state within 1 h, at which point the stable depth will be 0.04 m. The stabilization time of the upstream scouring hole is affected by v, which will gradually decrease from 15 h to 3 h with the increase in v. When v > 0.45 m/s, the upstream scouring hole is going to expand continuously. With the increase in v, its average development velocity increases from 6.68 cm/h to 8.66 cm/h, and its terrain changes to deep on the left and to shallow on the right. When the submarine cable is spanning, special attention should be paid to the depth of the scouring hole at the wake position. Throughout whole scouring process, the scouring hole at the wake position continues to develop and does not reach a stable state. With the increase in v, the depth of scouring hole at the wake position will increase from 14 cm to 20 cm, and the average development velocity will increase from 0.91 cm/h to 10.43 cm/h. As v increases, the time required to stabilize the downstream scouring hole is shortened from 1to 2 h to less than 1 h, but the stable depth is remains nearly constant at 13.5 cm.

An increase in v will increase the shear velocity. Therefore, when the depth of the scouring hole increases, the shear velocity in the hole will also increase, which can deepen both the upstream and downstream scouring hole. According to Equation (1), the Shields number is proportional to the square of the shear velocity. The increase in shear velocity significantly intensifies local scouring, which increases the development rate of scouring holes at the wake position and downstream.

4.3. Variation Rule of Spanning Time

In this paper, the spanning time is defined as the time taken for a semi-exposed submarine cable (initial state) to become a spanning submarine cable. Figure 10 illustrates the effect of the above parameters on the spanning time of the semi-exposed submarine cable.

Jmse 11 01349 g010 550

Figure 10. Influence of different parameters on spanning time of the semi-exposed submarine cable: (a) Sediment critical Shields number; (b) Sediment density; and (c) Ocean current velocity.From Figure 10a, the spanning time monotonically increases with the increase in the critical Shields number of sediment. However, the slope of the curve decreases first and then increases, and the inflection point is at 

θcr = 4.59 × 10

−2. The relationship between spanning time t and sediment’s critical Shields number 

θcr can be formulated by a cubic function as shown in Equation (6):

𝑡=−2.98+6.76𝜃𝑐𝑟−1.45𝜃2𝑐𝑟+0.11𝜃3𝑐𝑟.�=−2.98+6.76���−1.45���2+0.11���3.(6)It can be seen from Figure 10b that with the increase in the sediment density, the spanning time increases monotonically and linearly. The relationship between the spanning time t and the sediment’s density 

ρs can be formulated by the first order function as shown in Equation (7):

𝑡=−41.59+30.54𝜌𝑠.�=−41.59+30.54��.(7)Figure 10c shows that with the increase in the ocean current velocity, the spanning time decreases monotonically. The slope of the curve increases with the increase in the ocean current velocity, so it can be considered that there is saturation of the ocean current velocity effect. The relationship between the spanning time t and the ocean current velocity v can be formulated by the exponential function

𝑡=0.15𝑣−4.38.�=0.15�−4.38.(8)

5. Conclusions

In this paper, a three-dimensional CFD finite element numerical simulation model is established, which is used to research the local scouring process of the semi-exposed submarine cable under the steady-state ocean current. The relationship between shear velocity and scouring terrain is discussed, the influence of sediment critical Shields number, sediment density and ocean current velocity on the local scouring process is analyzed, and the variation rules of the spanning time of the semi-exposed submarine cable is given. The conclusions are as follows:

  • Under the steady-state ocean currents, scouring holes will be formed at the upstream, wake position and downstream of the semi-exposed submarine cable. The upstream and downstream scouring holes develop faster, which will reach a temporary stable state at about 1 h after the start of the scouring. The scouring hole at the wake position will continue to expand at a slower rate and eventually lead to the spanning of the submarine cable.
  • There is a close relationship between the distribution of shear velocity and the scouring terrain. As the local scouring process occurs, the location of the maximum shear velocity within the scouring hole shifts and causes the bottom of the hole to move as well.
  • When the sediment’s critical Shields number and density are significantly large and ocean current velocity is sufficiently low, the duration of the stable state of the upstream scouring hole will be prolonged, and the average development velocity of the scouring holes at the wake position and downstream will be reduced.
  • The relationship between the spanning time and the critical Shields number θcr can be formulated as a cubic function, in which the curve’s inflection point is θcr = 4.59 × 10−2. The relationship between spanning time and sediment density can be formulated as a linear function. The relationship between spanning time and ocean current velocity can be formulated by exponential function.

Based on the conclusions of this paper, even when it is too late to take measures or when the exposed position of the submarine cable cannot be located, the degree of burial depth development still can be predicted. This prediction is important for the operation and maintenance of the submarine cable. However, the study still leaves something to be desired. Only the local scouring process under the steady-state ocean current was studied, which is an extreme condition. In practice, exposed submarine cables are more likely to be scoured by reciprocating ocean currents. In the future, we will investigate the local scouring of submarine cables under the reciprocating ocean current.

Author Contributions

Conceptualization, Y.H. and Q.L.; methodology, Q.L., P.Z. and H.T.; software, Q.L.; validation, Q.L., L.C. and W.T.; writing—original draft preparation, Q.L.; writing—review and editing, Y.H. and Q.L.; supervision, Y.H. and L.Y. All authors have read and agreed to the published version of the manuscript.

Funding

This research was funded by the [Smart Grid Joint Fund Key Project between National Natural Science Foundation of China and State Grid Corporation] grant number [U1766220].

Institutional Review Board Statement

Not applicable.

Informed Consent Statement

Not applicable.

Data Availability Statement

The data supporting the reported results cannot be shared at this time, as they have been used in producing more publications on this research.

Acknowledgments

This work is supported by the Smart Grid Joint Fund Key Project of the National Natural Science Foundation of China and State Grid Corporation (Grant No. U1766220).

Conflicts of Interest

The authors declare no conflict of interest.

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Validity evaluation of popular liquid-vapor phase change models for cryogenic self-pressurization process

극저온 자체 가압 공정을 위한 인기 있는 액체-증기 상 변화 모델의 타당성 평가

액체-증기 상 변화 모델은 밀폐된 용기의 자체 가압 프로세스 시뮬레이션에 매우 큰 영향을 미칩니다. Hertz-Knudsen 관계, 에너지 점프 모델 및 그 파생물과 같은 널리 사용되는 액체-증기 상 변화 모델은 실온 유체를 기반으로 개발되었습니다. 액체-증기 전이를 통한 극저온 시뮬레이션에 널리 적용되었지만 각 모델의 성능은 극저온 조건에서 명시적으로 조사 및 비교되지 않았습니다. 본 연구에서는 171가지 일반적인 액체-증기 상 변화 모델을 통합한 통합 다상 솔버가 제안되었으며, 이를 통해 이러한 모델을 실험 데이터와 직접 비교할 수 있습니다. 증발 및 응축 모델의 예측 정확도와 계산 속도를 평가하기 위해 총 <>개의 자체 가압 시뮬레이션이 수행되었습니다. 압력 예측은 최적화 전략이 서로 다른 모델 계수에 크게 의존하는 것으로 나타났습니다. 에너지 점프 모델은 극저온 자체 가압 시뮬레이션에 적합하지 않은 것으로 나타났습니다. 평균 편차와 CPU 소비량에 따르면 Lee 모델과 Tanasawa 모델은 다른 모델보다 안정적이고 효율적인 것으로 입증되었습니다.

Elsevier

International Journal of Heat and Mass Transfer

Volume 181, December 2021, 121879

International Journal of Heat and Mass Transfer

Validity evaluation of popular liquid-vapor phase change models for cryogenic self-pressurization process

Author links open overlay panelZhongqi Zuo, Jingyi Wu, Yonghua HuangShow moreAdd to MendeleyShareCite

https://doi.org/10.1016/j.ijheatmasstransfer.2021.121879Get rights and content

Abstract

Liquid-vapor phase change models vitally influence the simulation of self-pressurization processes in closed containers. Popular liquid-vapor phase change models, such as the Hertz-Knudsen relation, energy jump model, and their derivations were developed based on room-temperature fluids. Although they had widely been applied in cryogenic simulations with liquid-vapor transitions, the performance of each model was not explicitly investigated and compared yet under cryogenic conditions. A unified multi-phase solver incorporating four typical liquid-vapor phase change models has been proposed in the present study, which enables direct comparison among those models against experimental data. A total number of 171 self-pressurization simulations were conducted to evaluate the evaporation and condensation models’ prediction accuracy and calculation speed. It was found that the pressure prediction highly depended on the model coefficients, whose optimization strategies differed from each other. The energy jump model was found inadequate for cryogenic self-pressurization simulations. According to the average deviation and CPU consumption, the Lee model and the Tanasawa model were proven to be more stable and more efficient than the others.

Introduction

The liquid-vapor phase change of cryogenic fluids is widely involved in industrial applications, such as the hydrogen transport vehicles [1], shipborne liquid natural gas (LNG) containers [2] and on-orbit cryogenic propellant tanks [3]. These applications require cryogenic fluids to be stored for weeks to months. Although high-performance insulation measures are adopted, heat inevitably enters the tank via radiation and conduction. The self-pressurization in the tank induced by the heat leakage eventually causes the venting loss of the cryogenic fluids and threatens the safety of the craft in long-term missions. To reduce the boil-off loss and extend the cryogenic storage duration, a more comprehensive understanding of the self-pressurization mechanism is needed.

Due to the difficulties and limitations in implementing cryogenic experiments, numerical modeling is a convenient and powerful way to study the self-pressurization process of cryogenic fluids. However, how the phase change models influence the mass and heat transfer under cryogenic conditions is still unsettled [4]. As concluded by Persad and Ward [5], a seemingly slight variation in the liquid-vapor phase change models can lead to erroneous predictions.

Among the liquid-vapor phase change models, the kinetic theory gas (KTG) based models and the energy jump model are the most popular ones used in recent self-pressurization simulations [6]. The KTG based models, also known as the Hertz-Knudsen relation models, were developed on the concept of the Maxwell-Boltzmann distribution of the gas molecular [7]. The Hertz-Knudsen relation has evolved to several models, including the Schrage model [8], the Tanasawa model [9], the Lee model [10] and the statistical rate theory (SRT) [11], which will be described in Section 2.2. Since the Schrage model and the Lee model are embedded and configured as the default ones in the commercial CFD solvers Flow-3D® and Ansys Fluent® respectively, they have been widely used in self-pressurization simulations for liquid nitrogen [12], [13] and liquid hydrogen [14], [15]. The major drawback of the KTG models lies in the difficulty of selecting model coefficients, which were reported in a considerably wide range spanning three magnitudes even for the same working fluid [16], [17], [18], [19], [20], [21]. Studies showed that the liquid level, pressure and mass transfer rate are directly influenced by the model coefficients [16], [22], [23], [24], [25]. Wrong coefficients will lead to deviation or even divergence of the results. The energy jump model is also known as the thermal limitation model. It assumes that the evaporation and condensation at the liquid-vapor interface are induced only by heat conduction. The model is widely adopted in lumped node simulations due to its simplicity [6], [26], [27]. To improve the accuracy of mass flux prediction, the energy jump model was modified by including the convection heat transfer [28], [29]. However, the convection correlations are empirical and developed mainly for room-temperature fluids. Whether the correlation itself can be precisely applied in cryogenic simulations still needs further investigation.

Fig. 1 summarizes the cryogenic simulations involving the modeling of evaporation and condensation processes in recent years. The publication has been increasing rapidly. However, the characteristics of each evaporation and condensation model are not explicitly revealed when simulating self-pressurization. A comparative study of the phase change models is highly needed for cryogenic fluids for a better simulation of the self-pressurization processes.

In the present paper, a unified multi-phase solver incorporating four typical liquid-vapor phase change models, namely the Tanasawa model, the Lee model, the energy jump model, and the modified energy jump model has been proposed, which enables direct comparison among different models. The models are used to simulate the pressure and temperature evolutions in an experimental liquid nitrogen tank in normal gravity, which helps to evaluate themselves in the aspects of accuracy, calculation speed and robustness.

Section snippets

Governing equations for the self-pressurization tank

In the present study, both the fluid domain and the solid wall of the tank are modeled and discretized. The heat transportation at the solid boundaries is considered to be irrelevant with the nearby fluid velocity. Consequently, two sets of the solid and the fluid governing equations can be decoupled and solved separately. The pressures in the cryogenic container are usually from 100 kPa to 300 kPa. Under these conditions, the Knudsen number is far smaller than 0.01, and the fluids are

Self-pressurization results and phase change model comparison

This section compares the simulation results by different phase change models. Section 3.1 compares the pressure and temperature outputs from two KTG based models, namely the Lee model and the Tanasawa model. Section 3.2 presents the pressure predictions from the energy transport models, namely the energy jump model and the modified energy jump model, and compares pressure prediction performances between the KTG based models and the energy transport models. Section 3.3 evaluates the four models 

Conclusion

A unified vapor-liquid-solid multi-phase numerical solver has been accomplished for the self pressurization simulation in cryogenic containers. Compared to the early fluid-only solver, the temperature prediction in the vicinity of the tank wall improves significantly. Four liquid-vapor phase change models were integrated into the solver, which enables fair and effective comparison for performances between each other. The pressure and temperature prediction accuracies, and the calculation speed

CRediT authorship contribution statement

Zhongqi Zuo: Data curation, Formal analysis, Writing – original draft, Validation. Jingyi Wu: Conceptualization, Writing – review & editing, Validation. Yonghua Huang: Conceptualization, Formal analysis, Writing – review & editing, Validation.

Declaration of Competing Interest

Authors declare that they have no financial and personal relationships with other people or organizations that can inappropriately influence our work, there is no professional or other personal interest of any nature or kind in any product, service and/or company that could be construed as influencing the position presented in, or the review of, the manuscript entitled, “Validity evaluation of popular liquid-vapor phase change models for cryogenic self-pressurization process”.

Acknowledgement

This project is supported by the National Natural Science Foundation of China (No. 51936006).

References (40)

There are more references available in the full text version of this article.

Cited by (7)

Intrusion of fine sediments into river bed and its effect on river environment – a research review

미세한 퇴적물이 강바닥에 침투하고 하천 환경에 미치는 영향 – 연구 검토

Intrusion of fine sediments into river bed and its effect on river environment – a research review

Nilav Karna,K.S. Hari Prasad, Sanjay Giri & A.S. Lodhi

Abstract

Fine sediments enter into the river through various sources such as channel bed, bank, and catchment. It has been regarded as a type of pollution in river. Fine sediments present in a river have a significant effect on river health. Benthic micro-organism, plants, and large fishes, all are part of food chain of river biota. Any detrimental effect on any of these components of food chain misbalances the entire riverine ecosystem. Numerous studies have been carried out on the various environmental aspects of rivers considering the presence of fine sediment in river flow. The present paper critically reviews many of these aspects to understand the various environmental impacts of suspended sediment on river health, flora and fauna.

Keywords: 

  1. Introduction
    The existence of fine sediment in a river system is a natural phenomenon. But in many cases it is exacerbated by the manmade activities. The natural cause of fines being in flow generally keeps the whole system in equilibrium except during some calamites whereas anthropogenic activities leading to fines entering into the flow puts several adverse impacts on the entire river system and its ecology. Presence of fines in flow is considered as a type of pollution in water. In United States,
    the fine sediment in water along with other non point source pollution is considered as a major obstacle in providing quality water for fishes and recreation activities (Diplas and Parker 1985).
    Sediments in a river are broadly of two types, organic and inorganic, and they both move in two ways either along the bed of the channel called bed load or in suspension called suspended load and their movements depend upon fluid flow and sediment characteristics. Further many investigators have divided the materials in suspension into two different types.
    One which originates from channel bed and bank is called bed material suspended load and another that migrates from feeding catchment area is called wash load. A general perception is that wash loads are very fine materials like clay, silt but it may not always be true (Woo et al. 1986). In general, suspended materials are of size less than 2 mm. The impact of sand on the various aspects of river is comparatively less than that of silt and clay. The latter are chemically active and good carrier of many contaminants and nutrients such as dioxins, phosphorous, heavy and trace metals, polychlorinated biphenyl (PCBs), radionuclide, etc. (Foster and Charlesworth 1996; Horowitz et al. 1995; Owens et al. 2001; Salomons and Förstner 1984; Stone and Droppo 1994; Thoms 1987). Foy and Bailey-Watt (1998) reported that out of 129 lakes in England and Wales, 69% have phosphorous contamination. Ten percent lakes, rivers, and bays of United States have sediment contaminants with chemicals as reported by USEPA. Several field and experimental studies have been conducted
    considering, sand, silt, and clay as suspended material. Hence, the subject reported herein is based on considering the fine sediment size smaller than 2 mm.
    Fine sediments have the ability to alter the hydraulics of the flow. Presence of fines in flow can change the magnitude of turbulence, it can change the friction resistance to flow. Fines can change the mobility and permeability of the bed material. In some extreme cases, fines in flow may even change the morphology of the river (Doeg and Koehn 1994; Nuttall 1972; Wright and Berrie 1987). Fines in the flow adversely affect the producer by increasing the turbidity, hindering the
    photosynthesis process by limiting the light penetration. This is ultimately reflected in the entire food ecosystem of river (Davis-Colley et al. 1992; Van Niewenhuyre and Laparrieve 1986). In addition, abrasion due to flowing sediment kills the aquatic flora (Edwards 1969; Brookes 1986). Intrusion of fines into the pores of river bed reduces space for several invertebrates, affects the spawning process (Petts 1984; Richards and Bacon 1994; Schalchli 1992). There are several other direct
    or indirect, short-term or long-term impacts of fines in river.
    The present paper reports the physical/environmental significance of fines in river. The hydraulic significance of presence of fines in the river has been reviewed in another paper (Effect of fine sediments on river hydraulics – a research review – http://dx.doi.org/10.1080/09715010.2014.982001).

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Effects of pile-cap elevation on scour and turbulence around a complex bridge pier

복잡한 교각 주변의 세굴 및 난기류에 대한 말뚝 뚜껑 높이의 영향

ABSTRACT

이 연구에서는 세 가지 다른 말뚝 뚜껑 높이에서 직사각형 말뚝 캡이 있는 복잡한 부두 주변의 지역 세굴 및 관련 흐름 유체 역학을 조사합니다. 말뚝 캡 높이가 초기 모래층에 대해 선택되었으며, 말뚝 캡이 흐름에 노출되지 않고(사례 I), 부분적으로 노출되고(사례 II) 완전히 노출(사례 III)되도록 했습니다. 실험은 맑은 물 세굴 조건 하에서 재순환 수로에서 수행되었으며, 입자 이미지 유속계 (PIV) 기술을 사용하여 다른 수직면에서 순간 유속을 얻었습니다. 부분적으로 노출된 파일 캡 케이스는 최대 수세미 깊이(MSD)를 보여주었습니다. 사례 II에서 MSD가 발생한 이유는 난류 유동장 분석을 통해 밝혀졌는데, 이는 말뚝 캡이 흐름에 노출됨에 따라 더 높은 세굴 깊이를 담당하는 말뚝 가장자리에서 와류 생성에 지배적으로 영향을 미친다는 것을 보여주었습니다. 유동장에 대한 파일 캡의 영향은 평균 속도, 소용돌이, 레이놀즈 전단 응력 및 난류 운동 에너지 윤곽을 통해 사례 III에서 두드러지게 나타났지만 파일 캡이 베드에서 떨어져 있었기 때문에 파일 캡 모서리는 수세미에 직접적인 영향을 미치지 않았습니다.

In this study, the local scour and the associated flow hydrodynamics around a complex pier with rectangular pile-cap at three different pile-cap elevations are investigated. The pile-cap elevations were selected with respect to the initial sand bed, such that the pile-cap was unexposed (case I), partially exposed (case II), and fully exposed (case III) to the flow. The experiments were performed in a recirculating flume under clear-water scour conditions, and the instantaneous flow velocity was obtained at different vertical planes using the particle image velocimetry (PIV) technique. The partially exposed pile-cap case showed the maximum obtained scour-depth (MSD). The reason behind the MSD occurrence in case II was enunciated through the analysis of turbulent flow field which showed that as the pile-cap got exposed to the flow, it dominantly affected the generation of vortices from the pile-cap corners responsible for the higher scour depth. The effect of the pile-cap on the flow field was prominently seen in case III through the mean velocities, vorticity, Reynolds shear stresses and turbulent kinetic energy contours, but since the pile-cap was away from the bed, the pile-cap corners did not show any direct effect on the scour.

KEYWORDS: 

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Figure 11. Sketch of scour mechanism around USAF under random waves.

Scour Characteristics and Equilibrium Scour Depth Prediction around Umbrella Suction Anchor Foundation under Random Waves

by Ruigeng Hu 1,Hongjun Liu 2,Hao Leng 1,Peng Yu 3 andXiuhai Wang 1,2,*

1College of Environmental Science and Engineering, Ocean University of China, Qingdao 266000, China

2Key Lab of Marine Environment and Ecology (Ocean University of China), Ministry of Education, Qingdao 266000, China

3Qingdao Geo-Engineering Survering Institute, Qingdao 266100, China

*Author to whom correspondence should be addressed.

J. Mar. Sci. Eng. 20219(8), 886; https://doi.org/10.3390/jmse9080886

Received: 6 July 2021 / Revised: 8 August 2021 / Accepted: 13 August 2021 / Published: 17 August 2021

(This article belongs to the Section Ocean Engineering)

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Abstract

A series of numerical simulation were conducted to study the local scour around umbrella suction anchor foundation (USAF) under random waves. In this study, the validation was carried out firstly to verify the accuracy of the present model. Furthermore, the scour evolution and scour mechanism were analyzed respectively. In addition, two revised models were proposed to predict the equilibrium scour depth Seq around USAF. At last, a parametric study was carried out to study the effects of the Froude number Fr and Euler number Eu for the Seq. The results indicate that the present numerical model is accurate and reasonable for depicting the scour morphology under random waves. The revised Raaijmakers’s model shows good agreement with the simulating results of the present study when KCs,p < 8. The predicting results of the revised stochastic model are the most favorable for n = 10 when KCrms,a < 4. The higher Fr and Eu both lead to the more intensive horseshoe vortex and larger Seq.

Keywords: 

scournumerical investigationrandom wavesequilibrium scour depthKC number

1. Introduction

The rapid expansion of cities tends to cause social and economic problems, such as environmental pollution and traffic jam. As a kind of clean energy, offshore wind power has developed rapidly in recent years. The foundation of offshore wind turbine (OWT) supports the upper tower, and suffers the cyclic loading induced by waves, tides and winds, which exerts a vital influence on the OWT system. The types of OWT foundation include the fixed and floating foundation, and the fixed foundation was used usually for nearshore wind turbine. After the construction of fixed foundation, the hydrodynamic field changes in the vicinity of the foundation, leading to the horseshoe vortex formation and streamline compression at the upside and sides of foundation respectively [1,2,3,4]. As a result, the neighboring soil would be carried away by the shear stress induced by vortex, and the scour hole would emerge in the vicinity of foundation. The scour holes increase the cantilever length, and weaken the lateral bearing capacity of foundation [5,6,7,8,9]. Moreover, the natural frequency of OWT system increases with the increase of cantilever length, causing the resonance occurs when the system natural frequency equals the wave or wind frequency [10,11,12]. Given that, an innovative foundation called umbrella suction anchor foundation (USAF) has been designed for nearshore wind power. The previous studies indicated the USAF was characterized by the favorable lateral bearing capacity with the low cost [6,13,14]. The close-up of USAF is shown in Figure 1, and it includes six parts: 1-interal buckets, 2-external skirt, 3-anchor ring, 4-anchor branch, 5-supporting rod, 6-telescopic hook. The detailed description and application method of USAF can be found in reference [13].

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Figure 1. The close-up of umbrella suction anchor foundation (USAF).

Numerical and experimental investigations of scour around OWT foundation under steady currents and waves have been extensively studied by many researchers [1,2,15,16,17,18,19,20,21,22,23,24]. The seabed scour can be classified as two types according to Shields parameter θ, i.e., clear bed scour (θ < θcr) or live bed scour (θ > θcr). Due to the set of foundation, the adverse hydraulic pressure gradient exists at upstream foundation edges, resulting in the streamline separation between boundary layer flow and seabed. The separating boundary layer ascended at upstream anchor edges and developed into the horseshoe vortex. Then, the horseshoe vortex moved downstream gradually along the periphery of the anchor, and the vortex shed off continually at the lee-side of the anchor, i.e., wake vortex. The core of wake vortex is a negative pressure center, liking a vacuum cleaner. Hence, the soil particles were swirled into the negative pressure core and carried away by wake vortexes. At the same time, the onset of scour at rear side occurred. Finally, the wake vortex became downflow when the turbulence energy could not support the survival of wake vortex. According to Tavouktsoglou et al. [25], the scale of pile wall boundary layer is proportional to 1/ln(Rd) (Rd is pile Reynolds), which means the turbulence intensity induced by the flow-structure interaction would decrease with Rd increases, but the effects of Rd can be neglected only if the flow around the foundation is fully turbulent [26]. According to previous studies [1,15,27,28,29,30,31,32], the scour development around pile foundation under waves was significantly influenced by Shields parameter θ and KC number simultaneously (calculated by Equation (1)). Sand ripples widely existed around pile under waves in the case of live bed scour, and the scour morphology is related with θ and KC. Compared with θKC has a greater influence on the scour morphology [21,27,28]. The influence mechanism of KC on the scour around the pile is reflected in two aspects: the horseshoe vortex at upstream and wake vortex shedding at downstream.

KC=UwmTD��=�wm��(1)

where, Uwm is the maximum velocity of the undisturbed wave-induced oscillatory flow at the sea bottom above the wave boundary layer, T is wave period, and D is pile diameter.

There are two prerequisites to satisfy the formation of horseshoe vortex at upstream pile edges: (1) the incoming flow boundary layer with sufficient thickness and (2) the magnitude of upstream adverse pressure gradient making the boundary layer separating [1,15,16,18,20]. The smaller KC results the lower adverse pressure gradient, and the boundary layer cannot separate, herein, there is almost no horseshoe vortex emerging at upside of pile. Sumer et al. [1,15] carried out several sets of wave flume experiments under regular and irregular waves respectively, and the experiment results show that there is no horseshoe vortex when KC is less than 6. While the scale and lifespan of horseshoe vortex increase evidently with the increase of KC when KC is larger than 6. Moreover, the wake vortex contributes to the scour at lee-side of pile. Similar with the case of horseshoe vortex, there is no wake vortex when KC is less than 6. The wake vortex is mainly responsible for scour around pile when KC is greater than 6 and less than O(100), while horseshoe vortex controls scour nearly when KC is greater than O(100).

Sumer et al. [1] found that the equilibrium scour depth was nil around pile when KC was less than 6 under regular waves for live bed scour, while the equilibrium scour depth increased with the increase of KC. Based on that, Sumer proposed an equilibrium scour depth predicting equation (Equation (2)). Carreiras et al. [33] revised Sumer’s equation with m = 0.06 for nonlinear waves. Different with the findings of Sumer et al. [1] and Carreiras et al. [33], Corvaro et al. [21] found the scour still occurred for KC ≈ 4, and proposed the revised equilibrium scour depth predicting equation (Equation (3)) for KC > 4.

Rudolph and Bos [2] conducted a series of wave flume experiments to investigate the scour depth around monopile under waves only, waves and currents combined respectively, indicting KC was one of key parameters in influencing equilibrium scour depth, and proposed the equilibrium scour depth predicting equation (Equation (4)) for low KC (1 < KC < 10). Through analyzing the extensive data from published literatures, Raaijmakers and Rudolph [34] developed the equilibrium scour depth predicting equation (Equation (5)) for low KC, which was suitable for waves only, waves and currents combined. Khalfin [35] carried out several sets of wave flume experiments to study scour development around monopile, and proposed the equilibrium scour depth predicting equation (Equation (6)) for low KC (0.1 < KC < 3.5). Different with above equations, the Khalfin’s equation considers the Shields parameter θ and KC number simultaneously in predicting equilibrium scour depth. The flow reversal occurred under through in one wave period, so sand particles would be carried away from lee-side of pile to upside, resulting in sand particles backfilled into the upstream scour hole [20,29]. Considering the backfilling effects, Zanke et al. [36] proposed the equilibrium scour depth predicting equation (Equation (7)) around pile by theoretical analysis, and the equation is suitable for the whole range of KC number under regular waves and currents combined.

S/D=1.3(1−exp([−m(KC−6)])�/�=1.3(1−exp(−�(��−6))(2)

where, m = 0.03 for linear waves.

S/D=1.3(1−exp([−0.02(KC−4)])�/�=1.3(1−exp(−0.02(��−4))(3)

S/D=1.3γKwaveKhw�/�=1.3��wave�ℎw(4)

where, γ is safety factor, depending on design process, typically γ = 1.5, Kwave is correction factor considering wave action, Khw is correction factor considering water depth.

S/D=1.5[tanh(hwD)]KwaveKhw�/�=1.5tanh(ℎw�)�wave�ℎw(5)

where, hw is water depth.

S/D=0.0753(θθcr−−−√−0.5)0.69KC0.68�/�=0.0753(��cr−0.5)0.69��0.68(6)

where, θ is shields parameter, θcr is critical shields parameter.

S/D=2.5(1−0.5u/uc)xrelxrel=xeff/(1+xeff)xeff=0.03(1−0.35ucr/u)(KC−6)⎫⎭⎬⎪⎪�/�=2.5(1−0.5�/��)��������=����/(1+����)����=0.03(1−0.35�cr/�)(��−6)(7)

where, u is near-bed orbital velocity amplitude, uc is critical velocity corresponding the onset of sediment motion.

S/D=1.3{1−exp[−0.03(KC2lnn+36)1/2−6]}�/�=1.31−exp−0.03(��2ln�+36)1/2−6(8)

where, n is the 1/n’th highest wave for random waves

For predicting equilibrium scour depth under irregular waves, i.e., random waves, Sumer and Fredsøe [16] found it’s suitable to take Equation (2) to predict equilibrium scour depth around pile under random waves with the root-mean-square (RMS) value of near-bed orbital velocity amplitude Um and peak wave period TP to calculate KC. Khalfin [35] recommended the RMS wave height Hrms and peak wave period TP were used to calculate KC for Equation (6). References [37,38,39,40] developed a series of stochastic theoretical models to predict equilibrium scour depth around pile under random waves, nonlinear random waves plus currents respectively. The stochastic approach thought the 1/n’th highest wave were responsible for scour in vicinity of pile under random waves, and the KC was calculated in Equation (8) with Um and mean zero-crossing wave period Tz. The results calculated by Equation (8) agree well with experimental values of Sumer and Fredsøe [16] if the 1/10′th highest wave was used. To author’s knowledge, the stochastic approach proposed by Myrhaug and Rue [37] is the only theoretical model to predict equilibrium scour depth around pile under random waves for the whole range of KC number in published documents. Other methods of predicting scour depth under random waves are mainly originated from the equation for regular waves-only, waves and currents combined, which are limited to the large KC number, such as KC > 6 for Equation (2) and KC > 4 for Equation (3) respectively. However, situations with relatively low KC number (KC < 4) often occur in reality, for example, monopile or suction anchor for OWT foundations in ocean environment. Moreover, local scour around OWT foundations under random waves has not yet been investigated fully. Therefore, further study are still needed in the aspect of scour around OWT foundations with low KC number under random waves. Given that, this study presents the scour sediment model around umbrella suction anchor foundation (USAF) under random waves. In this study, a comparison of equilibrium scour depth around USAF between this present numerical models and the previous theoretical models and experimental results was presented firstly. Then, this study gave a comprehensive analysis for the scour mechanisms around USAF. After that, two revised models were proposed according to the model of Raaijmakers and Rudolph [34] and the stochastic model developed by Myrhaug and Rue [37] respectively to predict the equilibrium scour depth. Finally, a parametric study was conducted to study the effects of the Froude number (Fr) and Euler number (Eu) to equilibrium scour depth respectively.

2. Numerical Method

2.1. Governing Equations of Flow

The following equations adopted in present model are already available in Flow 3D software. The authors used these theoretical equations to simulate scour in random waves without modification. The incompressible viscous fluid motion satisfies the Reynolds-averaged Navier-Stokes (RANS) equation, so the present numerical model solves RANS equations:

∂u∂t+1VF(uAx∂u∂x+vAy∂u∂y+wAz∂u∂z)=−1ρf∂p∂x+Gx+fx∂�∂�+1��(���∂�∂�+���∂�∂�+���∂�∂�)=−1�f∂�∂�+��+��(9)

∂v∂t+1VF(uAx∂v∂x+vAy∂v∂y+wAz∂v∂z)=−1ρf∂p∂y+Gy+fy∂�∂�+1��(���∂�∂�+���∂�∂�+���∂�∂�)=−1�f∂�∂�+��+��(10)

∂w∂t+1VF(uAx∂w∂x+vAy∂w∂y+wAz∂w∂z)=−1ρf∂p∂z+Gz+fz∂�∂�+1��(���∂�∂�+���∂�∂�+���∂�∂�)=−1�f∂�∂�+��+��(11)

where, VF is the volume fraction; uv, and w are the velocity components in xyz direction respectively with Cartesian coordinates; Ai is the area fraction; ρf is the fluid density, fi is the viscous fluid acceleration, Gi is the fluid body acceleration (i = xyz).

2.2. Turbulent Model

The turbulence closure is available by the turbulent model, such as one-equation, the one-equation k-ε model, the standard k-ε model, RNG k-ε turbulent model and large eddy simulation (LES) model. The LES model requires very fine mesh grid, so the computational time is large, which hinders the LES model application in engineering. The RNG k-ε model can reduce computational time greatly with high accuracy in the near-wall region. Furthermore, the RNG k-ε model computes the maximum turbulent mixing length dynamically in simulating sediment scour model. Therefore, the RNG k-ε model was adopted to study the scour around anchor under random waves [41,42].

∂kT∂T+1VF(uAx∂kT∂x+vAy∂kT∂y+wAz∂kT∂z)=PT+GT+DiffkT−εkT∂��∂�+1��(���∂��∂�+���∂��∂�+���∂��∂�)=��+��+������−���(12)

∂εT∂T+1VF(uAx∂εT∂x+vAy∂εT∂y+wAz∂εT∂z)=CDIS1εTkT(PT+CDIS3GT)+Diffε−CDIS2ε2TkT∂��∂�+1��(���∂��∂�+���∂��∂�+���∂��∂�)=����1����(��+����3��)+�����−����2��2��(13)

where, kT is specific kinetic energy involved with turbulent velocity, GT is the turbulent energy generated by buoyancy; εT is the turbulent energy dissipating rate, PT is the turbulent energy, Diffε and DiffkT are diffusion terms associated with VFAiCDIS1CDIS2 and CDIS3 are dimensionless parameters, and CDIS1CDIS3 have default values of 1.42, 0.2 respectively. CDIS2 can be obtained from PT and kT.

2.3. Sediment Scour Model

The sand particles may suffer four processes under waves, i.e., entrainment, bed load transport, suspended load transport, and deposition, so the sediment scour model should depict the above processes efficiently. In present numerical simulation, the sediment scour model includes the following aspects:

2.3.1. Entrainment and Deposition

The combination of entrainment and deposition determines the net scour rate of seabed in present sediment scour model. The entrainment lift velocity of sand particles was calculated as [43]:

ulift,i=αinsd0.3∗(θ−θcr)1.5∥g∥di(ρi−ρf)ρf−−−−−−−−−−−−√�lift,i=�����*0.3(�−�cr)1.5���(��−�f)�f(14)

where, αi is the entrainment parameter, ns is the outward point perpendicular to the seabed, d* is the dimensionless diameter of sand particles, which was calculated by Equation (15), θcr is the critical Shields parameter, g is the gravity acceleration, di is the diameter of sand particles, ρi is the density of seabed species.

d∗=di(∥g∥ρf(ρi−ρf)μ2f)1/3�*=��(��f(��−�f)�f2)1/3(15)

where μf is the fluid dynamic viscosity.

In Equation (14), the entrainment parameter αi confirms the rate at which sediment erodes when the given shear stress is larger than the critical shear stress, and the recommended value 0.018 was adopted according to the experimental data of Mastbergen and Von den Berg [43]. ns is the outward pointing normal to the seabed interface, and ns = (0,0,1) according to the Cartesian coordinates used in present numerical model.

The shields parameter was obtained from the following equation:

θ=U2f,m(ρi/ρf−1)gd50�=�f,m2(��/�f−1)��50(16)

where, Uf,m is the maximum value of the near-bed friction velocity; d50 is the median diameter of sand particles. The detailed calculation procedure of θ was available in Soulsby [44].

The critical shields parameter θcr was obtained from the Equation (17) [44]

θcr=0.31+1.2d∗+0.055[1−exp(−0.02d∗)]�cr=0.31+1.2�*+0.0551−exp(−0.02�*)(17)

The sand particles begin to deposit on seabed when the turbulence energy weaken and cann’t support the particles suspending. The setting velocity of the particles was calculated from the following equation [44]:

usettling,i=νfdi[(10.362+1.049d3∗)0.5−10.36]�settling,�=�f��(10.362+1.049�*3)0.5−10.36(18)

where νf is the fluid kinematic viscosity.

2.3.2. Bed Load Transport

This is called bed load transport when the sand particles roll or bounce over the seabed and always have contact with seabed. The bed load transport velocity was computed by [45]:

ubedload,i=qb,iδicb,ifb�bedload,�=�b,����b,��b(19)

where, qb,i is the bed load transport rate, which was obtained from Equation (20), δi is the bed load thickness, which was calculated by Equation (21), cb,i is the volume fraction of sand i in the multiple species, fb is the critical packing fraction of the seabed.

qb,i=8[∥g∥(ρi−ρfρf)d3i]1/2�b,�=8�(��−�f�f)��31/2(20)

δi=0.3d0.7∗(θθcr−1)0.5di��=0.3�*0.7(��cr−1)0.5��(21)

2.3.3. Suspended Load Transport

Through the following transport equation, the suspended sediment concentration could be acquired.

∂Cs,i∂t+∇(us,iCs,i)=∇∇(DfCs,i)∂�s,�∂�+∇(�s,��s,�)=∇∇(�f�s,�)(22)

where, Cs,i is the suspended sand particles mass concentration of sand i in the multiple species, us,i is the sand particles velocity of sand iDf is the diffusivity.

The velocity of sand i in the multiple species could be obtained from the following equation:

us,i=u¯¯+usettling,ics,i�s,�=�¯+�settling,��s,�(23)

where, u¯�¯ is the velocity of mixed fluid-particles, which can be calculated by the RANS equation with turbulence model, cs,i is the suspended sand particles volume concentration, which was computed from Equation (24).

cs,i=Cs,iρi�s,�=�s,���(24)

3. Model Setup

The seabed-USAF-wave three-dimensional scour numerical model was built using Flow-3D software. As shown in Figure 2, the model includes sandy seabed, USAF model, sea water, two baffles and porous media. The dimensions of USAF are shown in Table 1. The sandy bed (210 m in length, 30 m in width and 11 m in height) is made up of uniform fine sand with median diameter d50 = 0.041 cm. The USAF model includes upper steel tube with the length of 20 m, which was installed in the middle of seabed. The location of USAF is positioned at 140 m from the upstream inflow boundary and 70 m from the downstream outflow boundary. Two baffles were installed at two ends of seabed. In order to eliminate the wave reflection basically, the porous media was set at the outflow side on the seabed.

Jmse 09 00886 g002 550

Figure 2. (a) The sketch of seabed-USAF-wave three-dimensional model; (b) boundary condation:Wv-wave boundary, S-symmetric boundary, O-outflow boundary; (c) USAF model.

Table 1. Numerical simulating cases.

Table

3.1. Mesh Geometric Dimensions

In the simulation of the scour under the random waves, the model includes the umbrella suction anchor foundation, seabed and fluid. As shown in Figure 3, the model mesh includes global mesh grid and nested mesh grid, and the total number of grids is 1,812,000. The basic procedure for building mesh grid consists of two steps. Step 1: Divide the global mesh using regular hexahedron with size of 0.6 × 0.6. The global mesh area is cubic box, embracing the seabed and whole fluid volume, and the dimensions are 210 m in length, 30 m in width and 32 m in height. The details of determining the grid size can see the following mesh sensitivity section. Step 2: Set nested fine mesh grid in vicinity of the USAF with size of 0.3 × 0.3 so as to shorten the computation cost and improve the calculation accuracy. The encryption range is −15 m to 15 m in x direction, −15 m to 15 m in y direction and 0 m to 32 m in z direction, respectively. In order to accurately capture the free-surface dynamics, such as the fluid-air interface, the volume of fluid (VOF) method was adopted for tracking the free water surface. One specific algorithm called FAVORTM (Fractional Area/Volume Obstacle Representation) was used to define the fractional face areas and fractional volumes of the cells which are open to fluid flow.

Jmse 09 00886 g003 550

Figure 3. The sketch of mesh grid.

3.2. Boundary Conditions

As shown in Figure 2, the initial fluid length is 210 m as long as seabed. A wave boundary was specified at the upstream offshore end. The details of determining the random wave spectrum can see the following wave parameters section. The outflow boundary was set at the downstream onshore end. The symmetry boundary was used at the top and two sides of the model. The symmetric boundaries were the better strategy to improve the computation efficiency and save the calculation cost [46]. At the seabed bottom, the wall boundary was adopted, which means the u = v = w= 0. Besides, the upper steel tube of USAF was set as no-slip condition.

3.3. Wave Parameters

The random waves with JONSWAP wave spectrum were used for all simulations as realistic representation of offshore conditions. The unidirectional JONSWAP frequency spectrum was described as [47]:

S(ω)=αg2ω5exp[−54(ωpω)4]γexp[−(ω−ωp)22σ2ω2p]�(�)=��2�5exp−54(�p�)4�exp−(�−�p)22�2�p2(25)

where, α is wave energy scale parameter, which is calculated by Equation (26), ω is frequency, ωp is wave spectrum peak frequency, which can be obtained from Equation (27). γ is wave spectrum peak enhancement factor, in this study γ = 3.3. σ is spectral width factor, σ equals 0.07 for ω ≤ ωp and 0.09 for ω > ωp respectively.

α=0.0076(gXU2)−0.22�=0.0076(���2)−0.22(26)

ωp=22(gU)(gXU2)−0.33�p=22(��)(���2)−0.33(27)

where, X is fetch length, U is average wind velocity at 10 m height from mean sea level.

In present numerical model, the input key parameters include X and U for wave boundary with JONSWAP wave spectrum. The objective wave height and period are available by different combinations of X and U. In this study, we designed 9 cases with different wave heights, periods and water depths for simulating scour around USAF under random waves (see Table 2). For random waves, the wave steepness ε and Ursell number Ur were acquired form Equations (28) and (29) respectively

ε=2πgHsT2a�=2���s�a2(28)

Ur=Hsk2h3w�r=�s�2ℎw3(29)

where, Hs is significant wave height, Ta is average wave period, k is wave number, hw is water depth. The Shield parameter θ satisfies θ > θcr for all simulations in current study, indicating the live bed scour prevails.

Table 2. Numerical simulating cases.

Table

3.4. Mesh Sensitivity

In this section, a mesh sensitivity analysis was conducted to investigate the influence of mesh grid size to results and make sure the calculation is mesh size independent and converged. Three mesh grid size were chosen: Mesh 1—global mesh grid size of 0.75 × 0.75, nested fine mesh grid size of 0.4 × 0.4, and total number of grids 1,724,000, Mesh 2—global mesh grid size of 0.6 × 0.6, nested fine mesh grid size of 0.3 × 0.3, and total number of grids 1,812,000, Mesh 3—global mesh grid size of 0.4 × 0.4, nested fine mesh grid size of 0.2 × 0.2, and total number of grids 1,932,000. The near-bed shear velocity U* is an important factor for influencing scour process [1,15], so U* at the position of (4,0,11.12) was evaluated under three mesh sizes. As the Figure 4 shown, the maximum error of shear velocity ∆U*1,2 is about 39.8% between the mesh 1 and mesh 2, and 4.8% between the mesh 2 and mesh 3. According to the mesh sensitivity criterion adopted by Pang et al. [48], it’s reasonable to think the results are mesh size independent and converged with mesh 2. Additionally, the present model was built according to prototype size, and the mesh size used in present model is larger than the mesh size adopted by Higueira et al. [49] and Corvaro et al. [50]. If we choose the smallest cell size, it will take too much time. For example, the simulation with Mesh3 required about 260 h by using a computer with Intel Xeon Scalable Gold 4214 CPU @24 Cores, 2.2 GHz and 64.00 GB RAM. Therefore, in this case, considering calculation accuracy and computation efficiency, the mesh 2 was chosen for all the simulation in this study.

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Figure 4. Comparison of near-bed shear velocity U* with different mesh grid size.

The nested mesh block was adopted for seabed in vicinity of the USAF, which was overlapped with the global mesh block. When two mesh blocks overlap each other, the governing equations are by default solved on the mesh block with smaller average cell size (i.e., higher grid resolution). It is should be noted that the Flow 3D software used the moving mesh captures the scour evolution and automatically adjusts the time step size to be as large as possible without exceeding any of the stability limits, affecting accuracy, or unduly increasing the effort required to enforce the continuity condition [51].

3.5. Model Validation

In order to verify the reliability of the present model, the results of present study were compared with the experimental data of Khosronejad et al. [52]. The experiment was conducted in an open channel with a slender vertical pile under unidirectional currents. The comparison of scour development between the present results and the experimental results is shown in Figure 5. The Figure 5 reveals that the present results agree well with the experimental data of Khosronejad et al. [52]. In the first stage, the scour depth increases rapidly. After that, the scour depth achieves a maximum value gradually. The equilibrium scour depth calculated by the present model is basically corresponding with the experimental results of Khosronejad et al. [52], although scour depth in the present model is slightly larger than the experimental results at initial stage.

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Figure 5. Comparison of time evolution of scour between the present study and Khosronejad et al. [52], Petersen et al. [17].

Secondly, another comparison was further conducted between the results of present study and the experimental data of Petersen et al. [17]. The experiment was carried out in a flume with a circular vertical pile in combined waves and current. Figure 4 shows a comparison of time evolution of scour depth between the simulating and the experimental results. As Figure 5 indicates, the scour depth in this study has good overall agreement with the experimental results proposed in Petersen et al. [17]. The equilibrium scour depth calculated by the present model is 0.399 m, which equals to the experimental value basically. Overall, the above verifications prove the present model is accurate and capable in dealing with sediment scour under waves.

In addition, in order to calibrate and validate the present model for hydrodynamic parameters, the comparison of water surface elevation was carried out with laboratory experiments conducted by Stahlmann [53] for wave gauge No. 3. The Figure 6 depicts the surface wave profiles between experiments and numerical model results. The comparison indicates that there is a good agreement between the model results and experimental values, especially the locations of wave crest and trough. Comparison of the surface elevation instructs the present model has an acceptable relative error, and the model is a calibrated in terms of the hydrodynamic parameters.

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Figure 6. Comparison of surface elevation between the present study and Stahlmann [53].

Finally, another comparison was conducted for equilibrium scour depth or maximum scour depth under random waves with the experimental data of Sumer and Fredsøe [16] and Schendel et al. [22]. The Figure 7 shows the comparison between the numerical results and experimental data of Run01, Run05, Run21 and Run22 in Sumer and Fredsøe [16] and test A05 and A09 in Schendel et al. [22]. As shown in Figure 7, the equilibrium scour depth or maximum scour depth distributed within the ±30 error lines basically, meaning the reliability and accuracy of present model for predicting equilibrium scour depth around foundation in random waves. However, compared with the experimental values, the present model overestimated the equilibrium scour depth generally. Given that, a calibration for scour depth was carried out by multiplying the mean reduced coefficient 0.85 in following section.

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Figure 7. Comparison of equilibrium (or maximum) scour depth between the present study and Sumer and Fredsøe [16], Schendel et al. [22].

Through the various examination for hydrodynamic and morphology parameters, it can be concluded that the present model is a validated and calibrated model for scour under random waves. Thus, the present numerical model would be utilized for scour simulation around foundation under random waves.

4. Numerical Results and Discussions

4.1. Scour Evolution

Figure 8 displays the scour evolution for case 1–9. As shown in Figure 8a, the scour depth increased rapidly at the initial stage, and then slowed down at the transition stage, which attributes to the backfilling occurred in scour holes under live bed scour condition, resulting in the net scour decreasing. Finally, the scour reached the equilibrium state when the amount of sediment backfilling equaled to that of scouring in the scour holes, i.e., the net scour transport rate was nil. Sumer and Fredsøe [16] proposed the following formula for the scour development under waves

St=Seq(1−exp(−t/Tc))�t=�eq(1−exp(−�/�c))(30)

where Tc is time scale of scour process.

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Figure 8. Time evolution of scour for case 1–9: (a) Case 1–5; (b) Case 6–9.

The computing time is 3600 s and the scour development curves in Figure 8 kept fluctuating, meaning it’s still not in equilibrium scour stage in these cases. According to Sumer and Fredsøe [16], the equilibrium scour depth can be acquired by fitting the data with Equation (30). From Figure 8, it can be seen that the scour evolution obtained from Equation (30) is consistent with the present study basically at initial stage, but the scour depth predicted by Equation (30) developed slightly faster than the simulating results and the Equation (30) overestimated the scour depth to some extent. Overall, the whole tendency of the results calculated by Equation (30) agrees well with the simulating results of the present study, which means the Equation (30) is applicable to depict the scour evolution around USAF under random waves.

4.2. Scour Mechanism under Random Waves

The scour morphology and scour evolution around USAF are similar under random waves in case 1~9. Taking case 7 as an example, the scour morphology is shown in Figure 9.

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Figure 9. Scour morphology under different times for case 7.

From Figure 9, at the initial stage (t < 1200 s), the scour occurred at upstream foundation edges between neighboring anchor branches. The maximum scour depth appeared at the lee-side of the USAF. Correspondingly, the sediments deposited at the periphery of the USAF, and the location of the maximum accretion depth was positioned at an angle of about 45° symmetrically with respect to the wave propagating direction in the lee-side of the USAF. After that, when t > 2400 s, the location of the maximum scour depth shifted to the upside of the USAF at an angle of about 45° with respect to the wave propagating direction.

According to previous studies [1,15,16,19,30,31], the horseshoe vortex, streamline compression and wake vortex shedding were responsible for scour around foundation. The Figure 10 displays the distribution of flow velocity in vicinity of foundation, which reflects the evolving processes of horseshoe vertex.

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Figure 10. Velocity profile around USAF: (a) Flow runup and down stream at upstream anchor edges; (b) Horseshoe vortex at upstream anchor edges; (c) Flow reversal during wave through stage at lee side.

As shown in Figure 10, the inflow tripped to the upstream edges of the USAF and it was blocked by the upper tube of USAF. Then, the downflow formed the horizontal axis clockwise vortex and rolled on the seabed bypassing the tube, that is, the horseshoe vortex (Figure 11). The Figure 12 displays the turbulence intensity around the tube on the seabed. From Figure 12, it can be seen that the turbulence intensity was high-intensity with respect to the region of horseshoe vortex. This phenomenon occurred because of drastic water flow momentum exchanging in the horseshoe vortex. As a result, it created the prominent shear stress on the seabed, causing the local scour at the upstream edges of USAF. Besides, the horseshoe vortex moved downstream gradually along the periphery of the tube and the wake vortex shed off continually at the lee-side of the USAF, i.e., wake vortex.

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Figure 11. Sketch of scour mechanism around USAF under random waves.

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Figure 12. Turbulence intensity: (a) Turbulence intensity of horseshoe vortex; (b) Turbulence intensity of wake vortex; (c) Turbulence intensity of accretion area.

The core of wake vortex is a negative pressure center, liking a vacuum cleaner [11,42]. Hence, the soil particles were swirled into the negative pressure core and carried away by wake vortex. At the same time, the onset of scour at rear side occurred. Finally, the wake vortex became downflow at the downside of USAF. As is shown in Figure 12, the turbulence intensity was low where the downflow occurred at lee-side, which means the turbulence energy may not be able to support the survival of wake vortex, leading to accretion happening. As mentioned in previous section, the formation of horseshoe vortex was dependent with adverse pressure gradient at upside of foundation. As shown in Figure 13, the evaluated range of pressure distribution is −15 m to 15 m in x direction. The t = 450 s and t = 1800 s indicate that the wave crest and trough arrived at the upside and lee-side of the foundation respectively, and the t = 350 s was neither the wave crest nor trough. The adverse gradient pressure reached the maximum value at t = 450 s corresponding to the wave crest phase. In this case, it’s helpful for the wave boundary separating fully from seabed, which leads to the formation of horseshoe vortex with high turbulence intensity. Therefore, the horseshoe vortex is responsible for the local scour between neighboring anchor branches at upside of USAF. What’s more, due to the combination of the horseshoe vortex and streamline compression, the maximum scour depth occurred at the upside of the USAF with an angle of about 45° corresponding to the wave propagating direction. This is consistent with the findings of Pang et al. [48] and Sumer et al. [1,15] in case of regular waves. At the wave trough phase (t = 1800 s), the pressure gradient became positive at upstream USAF edges, which hindered the separating of wave boundary from seabed. In the meantime, the flow reversal occurred (Figure 10) and the adverse gradient pressure appeared at downstream USAF edges, but the magnitude of adverse gradient pressure at lee-side was lower than the upstream gradient pressure under wave crest. In this way, the intensity of horseshoe vortex behind the USAF under wave trough was low, which explains the difference of scour depth at upstream and downstream, i.e., the scour asymmetry. In other words, the scour asymmetry at upside and downside of USAF was attributed to wave asymmetry for random waves, and the phenomenon became more evident for nonlinear waves [21]. Briefly speaking, the vortex system at wave crest phase was mainly related to the scour process around USAF under random waves.

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Figure 13. Pressure distribution around USAF.

4.3. Equilibrium Scour Depth

The KC number is a key parameter for horseshoe vortex emerging and evolving under waves. According to Equation (1), when pile diameter D is fixed, the KC depends on the maximum near-bed velocity Uwm and wave period T. For random waves, the Uwm can be denoted by the root-mean-square (RMS) value of near-bed velocity amplitude Uwm,rms or the significant value of near-bed velocity amplitude Uwm,s. The Uwm,rms and Uwm,s for all simulating cases of the present study are listed in Table 3 and Table 4. The T can be denoted by the mean up zero-crossing wave period Ta, peak wave period Tp, significant wave period Ts, the maximum wave period Tm, 1/10′th highest wave period Tn = 1/10 and 1/5′th highest wave period Tn = 1/5 for random waves, so the different combinations of Uwm and T will acquire different KC. The Table 3 and Table 4 list 12 types of KC, for example, the KCrms,s was calculated by Uwm,rms and Ts. Sumer and Fredsøe [16] conducted a series of wave flume experiments to investigate the scour depth around monopile under random waves, and found the equilibrium scour depth predicting equation (Equation (2)) for regular waves was applicable for random waves with KCrms,p. It should be noted that the Equation (2) is only suitable for KC > 6 under regular waves or KCrms,p > 6 under random waves.

Table 3. Uwm,rms and KC for case 1~9.

Table

Table 4. Uwm,s and KC for case 1~9.

Table

Raaijmakers and Rudolph [34] proposed the equilibrium scour depth predicting model (Equation (5)) around pile under waves, which is suitable for low KC. The format of Equation (5) is similar with the formula proposed by Breusers [54], which can predict the equilibrium scour depth around pile at different scour stages. In order to verify the applicability of Raaijmakers’s model for predicting the equilibrium scour depth around USAF under random waves, a validation of the equilibrium scour depth Seq between the present study and Raaijmakers’s equation was conducted. The position where the scour depth Seq was evaluated is the location of the maximum scour depth, and it was depicted in Figure 14. The Figure 15 displays the comparison of Seq with different KC between the present study and Raaijmakers’s model.

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Figure 14. Sketch of the position where the Seq was evaluated.

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Figure 15. Comparison of the equilibrium scour depth between the present model and the model of Raaijmakers and Rudolph [34]: (aKCrms,sKCrms,a; (bKCrms,pKCrms,m; (cKCrms,n = 1/10KCrms,n = 1/5; (dKCs,sKCs,a; (eKCs,pKCs,m; (fKCs,n = 1/10KCs,n = 1/5.

As shown in Figure 15, there is an error in predicting Seq between the present study and Raaijmakers’s model, and Raaijmakers’s model underestimates the results generally. Although the error exists, the varying trend of Seq with KC obtained from Raaijmakers’s model is consistent with the present study basically. What’s more, the error is minimum and the Raaijmakers’s model is of relatively high accuracy for predicting scour around USAF under random waves by using KCs,p. Based on this, a further revision was made to eliminate the error as much as possible, i.e., add the deviation value ∆S/D in the Raaijmakers’s model. The revised equilibrium scour depth predicting equation based on Raaijmakers’s model can be written as

S′eq/D=1.95[tanh(hD)](1−exp(−0.012KCs,p))+ΔS/D�eq′/�=1.95tanh(ℎ�)(1−exp(−0.012��s,p))+∆�/�(31)

As the Figure 16 shown, through trial-calculation, when ∆S/D = 0.05, the results calculated by Equation (31) show good agreement with the simulating results of the present study. The maximum error is about 18.2% and the engineering requirements have been met basically. In order to further verify the accuracy of the revised model for large KC (KCs,p > 4) under random waves, a validation between the revised model and the previous experimental results [21]. The experiment was conducted in a flume (50 m in length, 1.0 m in width and 1.3 m in height) with a slender vertical pile (D = 0.1 m) under random waves. The seabed is composed of 0.13 m deep layer of sand with d50 = 0.6 mm and the water depth is 0.5 m for all tests. The significant wave height is 0.12~0.21 m and the KCs,p is 5.52~11.38. The comparison between the predicting results by Equation (31) and the experimental results of Corvaro et al. [21] is shown in Figure 17. From Figure 17, the experimental data evenly distributes around the predicted results and the prediction accuracy is favorable when KCs,p < 8. However, the gap between the predicting results and experimental data becomes large and the Equation (31) overestimates the equilibrium scour depth to some extent when KCs,p > 8.

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Figure 16. Comparison of Seq between the simulating results and the predicting values by Equation (31).

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Figure 17. Comparison of Seq/D between the Experimental results of Corvaro et al. [21] and the predicting values by Equation (31).

In ocean environment, the waves are composed of a train of sinusoidal waves with different frequencies and amplitudes. The energy of constituent waves with very large and very small frequencies is relatively low, and the energy of waves is mainly concentrated in a certain range of moderate frequencies. Myrhaug and Rue [37] thought the 1/n’th highest wave was responsible for scour and proposed the stochastic model to predict the equilibrium scour depth around pile under random waves for full range of KC. Noteworthy is that the KC was denoted by KCrms,a in the stochastic model. To verify the application of the stochastic model for predicting scour depth around USAF, a validation between the simulating results of present study and predicting results by the stochastic model with n = 2,3,5,10,20,500 was carried out respectively.

As shown in Figure 18, compared with the simulating results, the stochastic model underestimates the equilibrium scour depth around USAF generally. Although the error exists, the varying trend of Seq with KCrms,a obtained from the stochastic model is consistent with the present study basically. What’s more, the gap between the predicting values by stochastic model and the simulating results decreases with the increase of n, but for large n, for example n = 500, the varying trend diverges between the predicting values and simulating results, meaning it’s not feasible only by increasing n in stochastic model to predict the equilibrium scour depth around USAF.

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Figure 18. Comparison of Seq between the simulating results and the predicting values by Equation (8).

The Figure 19 lists the deviation value ∆Seq/D′ between the predicting values and simulating results with different KCrms,a and n. Then, fitted the relationship between the ∆S′and n under different KCrms,a, and the fitting curve can be written by Equation (32). The revised stochastic model (Equation (33)) can be acquired by adding ∆Seq/D′ to Equation (8).

ΔSeq/D=0.052*exp(−n/6.566)+0.068∆�eq/�=0.052*exp(−�/6.566)+0.068(32)

S′eq¯/D=S′eq/D+0.052*exp(−n/6.566)+0.068�eq′¯/�=�eq′/�+0.052*exp(−�/6.566)+0.068(33)

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Figure 19. The fitting line between ∆S′and n.

The comparison between the predicting results by Equation (33) and the simulating results of present study is shown in Figure 20. According to the Figure 20, the varying trend of Seq with KCrms,a obtained from the stochastic model is consistent with the present study basically. Compared with predicting results by the stochastic model, the results calculated by Equation (33) is favorable. Moreover, comparison with simulating results indicates that the predicting results are the most favorable for n = 10, which is consistent with the findings of Myrhaug and Rue [37] for equilibrium scour depth predicting around slender pile in case of random waves.

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Figure 20. Comparison of Seq between the simulating results and the predicting values by Equation (33).

In order to further verify the accuracy of the Equation (33) for large KC (KCrms,a > 4) under random waves, a validation was conducted between the Equation (33) and the previous experimental results of Sumer and Fredsøe [16] and Corvaro et al. [21]. The details of experiments conducted by Corvaro et al. [21] were described in above section. Sumer and Fredsøe [16] investigated the local scour around pile under random waves. The experiments were conducted in a wave basin with a slender vertical pile (D = 0.032, 0.055 m). The seabed is composed of 0.14 m deep layer of sand with d50 = 0.2 mm and the water depth was maintained at 0.5 m. The JONSWAP wave spectrum was used and the KCrms,a was 5.29~16.95. The comparison between the predicting results by Equation (33) and the experimental results of Sumer and Fredsøe [16] and Corvaro et al. [21] are shown in Figure 21. From Figure 21, contrary to the case of low KCrms,a (KCrms,a < 4), the error between the predicting values and experimental results increases with decreasing of n for KCrms,a > 4. Therefore, the predicting results are the most favorable for n = 2 when KCrms,a > 4.

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Figure 21. Comparison of Seq between the experimental results of Sumer and Fredsøe [16] and Corvaro et al. [21] and the predicting values by Equation (33).

Noteworthy is that the present model was built according to prototype size, so the errors between the numerical results and experimental data of References [16,21] may be attribute to the scale effects. In laboratory experiments on scouring process, it is typically impossible to ensure a rigorous similarity of all physical parameters between the model and prototype structure, leading to the scale effects in the laboratory experiments. To avoid a cohesive behaviour, the bed material was not scaled geometrically according to model scale. As a consequence, the relatively large-scaled sediments sizes may result in the overestimation of bed load transport and underestimation of suspended load transport compared with field conditions. What’s more, the disproportional scaled sediment presumably lead to the difference of bed roughness between the model and prototype, and thus large influences for wave boundary layer on the seabed and scour process. Besides, according to Corvaro et al. [21] and Schendel et al. [55], the pile Reynolds numbers and Froude numbers both affect the scour depth for the condition of non fully developed turbulent flow in laboratory experiments.

4.4. Parametric Study

4.4.1. Influence of Froude Number

As described above, the set of foundation leads to the adverse pressure gradient appearing at upstream, leading to the wave boundary layer separating from seabed, then horseshoe vortex formatting and the horseshoe vortex are mainly responsible for scour around foundation (see Figure 22). The Froude number Fr is the key parameter to influence the scale and intensity of horseshoe vortex. The Fr under waves can be calculated by the following formula [42]

Fr=UwgD−−−√�r=�w��(34)

where Uw is the mean water particle velocity during 1/4 cycle of wave oscillation, obtained from the following formula. Noteworthy is that the root-mean-square (RMS) value of near-bed velocity amplitude Uwm,rms is used for calculating Uwm.

Uw=1T/4∫0T/4Uwmsin(t/T)dt=2πUwm�w=1�/4∫0�/4�wmsin(�/�)��=2��wm(35)

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Figure 22. Sketch of flow field at upstream USAF edges.

Tavouktsoglou et al. [25] proposed the following formula between Fr and the vertical location of the stagnation y

yh∝Fer�ℎ∝�r�(36)

where e is constant.

The Figure 23 displays the relationship between Seq/D and Fr of the present study. In order to compare with the simulating results, the experimental data of Corvaro et al. [21] was also depicted in Figure 23. As shown in Figure 23, the equilibrium scour depth appears a logarithmic increase as Fr increases and approaches the mathematical asymptotic value, which is also consistent with the experimental results of Corvaro et al. [21]. According to Figure 24, the adverse pressure gradient pressure at upstream USAF edges increases with the increase of Fr, which is benefit for the wave boundary layer separating from seabed, resulting in the high-intensity horseshoe vortex, hence, causing intensive scour around USAF. Based on the previous study of Tavouktsoglou et al. [25] for scour around pile under currents, the high Fr leads to the stagnation point is closer to the mean sea level for shallow water, causing the stronger downflow kinetic energy. As mentioned in previous section, the energy of downflow at upstream makes up the energy of the subsequent horseshoe vortex, so the stronger downflow kinetic energy results in the more intensive horseshoe vortex. Therefore, the higher Fr leads to the more intensive horseshoe vortex by influencing the position of stagnation point y presumably. Qi and Gao [19] carried out a series of flume tests to investigate the scour around pile under regular waves, and proposed the fitting formula between Seq/D and Fr as following

lg(Seq/D)=Aexp(B/Fr)+Clg(�eq/�)=�exp(�/�r)+�(37)

where AB and C are constant.

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Figure 23. The fitting curve between Seq/D and Fr.

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Figure 24. Sketch of adverse pressure gradient at upstream USAF edges.

Took the Equation (37) to fit the simulating results with A = −0.002, B = 0.686 and C = −0.808, and the results are shown in Figure 23. From Figure 23, the simulating results evenly distribute around the Equation (37) and the varying trend of Seq/D and Fr in present study is consistent with Equation (37) basically, meaning the Equation (37) is applicable to express the relationship of Seq/D with Fr around USAF under random waves.

4.4.2. Influence of Euler Number

The Euler number Eu is the influencing factor for the hydrodynamic field around foundation. The Eu under waves can be calculated by the following formula. The Eu can be represented by the Equation (38) for uniform cylinders [25]. The root-mean-square (RMS) value of near-bed velocity amplitude Um,rms is used for calculating Um.

Eu=U2mgD�u=�m2��(38)

where Um is depth-averaged flow velocity.

The Figure 25 displays the relationship between Seq/D and Eu of the present study. In order to compare with the simulating results, the experimental data of Sumer and Fredsøe [16] and Corvaro et al. [21] were also plotted in Figure 25. As shown in Figure 25, similar with the varying trend of Seq/D and Fr, the equilibrium scour depth appears a logarithmic increase as Eu increases and approaches the mathematical asymptotic value, which is also consistent with the experimental results of Sumer and Fredsøe [16] and Corvaro et al. [21]. According to Figure 24, the adverse pressure gradient pressure at upstream USAF edges increases with the increasing of Eu, which is benefit for the wave boundary layer separating from seabed, inducing the high-intensity horseshoe vortex, hence, causing intensive scour around USAF.

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Figure 25. The fitting curve between Seq/D and Eu.

Therefore, the variation of Fr and Eu reflect the magnitude of adverse pressure gradient pressure at upstream. Given that, the Equation (37) also was used to fit the simulating results with A = 8.875, B = 0.078 and C = −9.601, and the results are shown in Figure 25. From Figure 25, the simulating results evenly distribute around the Equation (37) and the varying trend of Seq/D and Eu in present study is consistent with Equation (37) basically, meaning the Equation (37) is also applicable to express the relationship of Seq/D with Eu around USAF under random waves. Additionally, according to the above description of Fr, it can be inferred that the higher Fr and Eu both lead to the more intensive horseshoe vortex by influencing the position of stagnation point y presumably.

5. Conclusions

A series of numerical models were established to investigate the local scour around umbrella suction anchor foundation (USAF) under random waves. The numerical model was validated for hydrodynamic and morphology parameters by comparing with the experimental data of Khosronejad et al. [52], Petersen et al. [17], Sumer and Fredsøe [16] and Schendel et al. [22]. Based on the simulating results, the scour evolution and scour mechanisms around USAF under random waves were analyzed respectively. Two revised models were proposed according to the model of Raaijmakers and Rudolph [34] and the stochastic model developed by Myrhaug and Rue [37] to predict the equilibrium scour depth around USAF under random waves. Finally, a parametric study was carried out with the present model to study the effects of the Froude number Fr and Euler number Eu to the equilibrium scour depth around USAF under random waves. The main conclusions can be described as follows.(1)

The packed sediment scour model and the RNG k−ε turbulence model were used to simulate the sand particles transport processes and the flow field around UASF respectively. The scour evolution obtained by the present model agrees well with the experimental results of Khosronejad et al. [52], Petersen et al. [17], Sumer and Fredsøe [16] and Schendel et al. [22], which indicates that the present model is accurate and reasonable for depicting the scour morphology around UASF under random waves.(2)

The vortex system at wave crest phase is mainly related to the scour process around USAF under random waves. The maximum scour depth appeared at the lee-side of the USAF at the initial stage (t < 1200 s). Subsequently, when t > 2400 s, the location of the maximum scour depth shifted to the upside of the USAF at an angle of about 45° with respect to the wave propagating direction.(3)

The error is negligible and the Raaijmakers’s model is of relatively high accuracy for predicting scour around USAF under random waves when KC is calculated by KCs,p. Given that, a further revision model (Equation (31)) was proposed according to Raaijmakers’s model to predict the equilibrium scour depth around USAF under random waves and it shows good agreement with the simulating results of the present study when KCs,p < 8.(4)

Another further revision model (Equation (33)) was proposed according to the stochastic model established by Myrhaug and Rue [37] to predict the equilibrium scour depth around USAF under random waves, and the predicting results are the most favorable for n = 10 when KCrms,a < 4. However, contrary to the case of low KCrms,a, the predicting results are the most favorable for n = 2 when KCrms,a > 4 by the comparison with experimental results of Sumer and Fredsøe [16] and Corvaro et al. [21].(5)

The same formula (Equation (37)) is applicable to express the relationship of Seq/D with Eu or Fr, and it can be inferred that the higher Fr and Eu both lead to the more intensive horseshoe vortex and larger Seq.

Author Contributions

Conceptualization, H.L. (Hongjun Liu); Data curation, R.H. and P.Y.; Formal analysis, X.W. and H.L. (Hao Leng); Funding acquisition, X.W.; Writing—original draft, R.H. and P.Y.; Writing—review & editing, X.W. and H.L. (Hao Leng); The final manuscript has been approved by all the authors. All authors have read and agreed to the published version of the manuscript.

Funding

This research was funded by the Fundamental Research Funds for the Central Universities (grant number 202061027) and the National Natural Science Foundation of China (grant number 41572247).

Institutional Review Board Statement

Not applicable.

Informed Consent Statement

Not applicable.

Data Availability Statement

The data presented in this study are available on request from the corresponding author.

Conflicts of Interest

The authors declare no conflict of interest.

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Hu, R.; Liu, H.; Leng, H.; Yu, P.; Wang, X. Scour Characteristics and Equilibrium Scour Depth Prediction around Umbrella Suction Anchor Foundation under Random Waves. J. Mar. Sci. Eng. 20219, 886. https://doi.org/10.3390/jmse9080886

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Hu R, Liu H, Leng H, Yu P, Wang X. Scour Characteristics and Equilibrium Scour Depth Prediction around Umbrella Suction Anchor Foundation under Random Waves. Journal of Marine Science and Engineering. 2021; 9(8):886. https://doi.org/10.3390/jmse9080886Chicago/Turabian Style

Hu, Ruigeng, Hongjun Liu, Hao Leng, Peng Yu, and Xiuhai Wang. 2021. “Scour Characteristics and Equilibrium Scour Depth Prediction around Umbrella Suction Anchor Foundation under Random Waves” Journal of Marine Science and Engineering 9, no. 8: 886. https://doi.org/10.3390/jmse9080886

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Study on Hydrodynamic Performance of Unsymmetrical Double Vertical Slotted Barriers

침수된 강성 식생을 갖는 개방 수로 흐름의 특성에 대한 3차원 수치 시뮬레이션

A 3-D numerical simulation of the characteristics of open channel flows with submerged rigid vegetation

Journal of Hydrodynamics volume 33, pages833–843 (2021)

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Abstract

이 백서는 Flow-3D를 적용하여 다양한 흐름 배출 및 식생 시나리오가 흐름 속도(세로, 가로 및 수직 속도 포함)에 미치는 영향을 조사합니다.

실험적 측정을 통한 검증 후 식생직경, 식생높이, 유량방류량에 대한 민감도 분석을 수행하였다. 종방향 속도의 경우 흐름 구조에 가장 큰 영향을 미치는 것은 배출보다는 식생 직경에서 비롯됩니다.

그러나 식생 높이는 수직 분포의 변곡점을 결정합니다. 식생지 내 두 지점, 즉 상류와 하류의 횡속도를 비교하면 수심에 따른 대칭적인 패턴을 확인할 수 있다. 식생 지역의 가로 및 세로 유체 순환 패턴을 포함하여 흐름 또는 식생 시나리오와 관계없이 수직 속도에 대해서도 동일한 패턴이 관찰됩니다.

또한 식생의 직경이 클수록 이러한 패턴이 더 분명해집니다. 상부 순환은 초목 캐노피 근처에서 발생합니다. 식생지역의 가로방향과 세로방향의 순환에 관한 이러한 발견은 침수식생을 통한 3차원 유동구조를 밝혀준다.

This paper applies the Flow-3D to investigate the impacts of different flow discharge and vegetation scenarios on the flow velocity (including the longitudinal, transverse and vertical velocities). After the verification by using experimental measurements, a sensitivity analysis is conducted for the vegetation diameter, the vegetation height and the flow discharge. For the longitudinal velocity, the greatest impact on the flow structure originates from the vegetation diameter, rather than the discharge. The vegetation height, however, determines the inflection point of the vertical distribution. Comparing the transverse velocities at two positions in the vegetated area, i.e., the upstream and the downstream, a symmetric pattern is identified along the water depth. The same pattern is also observed for the vertical velocity regardless of the flow or vegetation scenario, including both transverse and vertical fluid circulation patterns in the vegetated area. Moreover, the larger the vegetation diameter is, the more evident these patterns become. The upper circulation occurs near the vegetation canopy. These findings regarding the circulations along the transverse and vertical directions in the vegetated region shed light on the 3-D flow structure through the submerged vegetation.

Key words

  • Submerged rigid vegetation
  • longitudinal velocity
  • transverse velocity
  • vertical velocity
  • open channel

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Figure 2 Modeling the plant with cylindrical tubes at the bottom of the canal.

Optimized Vegetation Density to Dissipate Energy of Flood Flow in Open Canals

열린 운하에서 홍수 흐름의 에너지를 분산시키기 위해 최적화된 식생 밀도

Mahdi Feizbahr,1Navid Tonekaboni,2Guang-Jun Jiang,3,4and Hong-Xia Chen3,4
Academic Editor: Mohammad Yazdi

Abstract

강을 따라 식생은 조도를 증가시키고 평균 유속을 감소시키며, 유동 에너지를 감소시키고 강 횡단면의 유속 프로파일을 변경합니다. 자연의 많은 운하와 강은 홍수 동안 초목으로 덮여 있습니다. 운하의 조도는 식물의 영향을 많이 받기 때문에 홍수시 유동저항에 큰 영향을 미친다. 식물로 인한 흐름에 대한 거칠기 저항은 흐름 조건과 식물에 따라 달라지므로 모델은 유속, 유속 깊이 및 수로를 따라 식생 유형의 영향을 고려하여 유속을 시뮬레이션해야 합니다. 총 48개의 모델을 시뮬레이션하여 근관의 거칠기 효과를 조사했습니다. 결과는 속도를 높임으로써 베드 속도를 감소시키는 식생의 영향이 무시할만하다는 것을 나타냅니다.

Abstract

Vegetation along the river increases the roughness and reduces the average flow velocity, reduces flow energy, and changes the flow velocity profile in the cross section of the river. Many canals and rivers in nature are covered with vegetation during the floods. Canal’s roughness is strongly affected by plants and therefore it has a great effect on flow resistance during flood. Roughness resistance against the flow due to the plants depends on the flow conditions and plant, so the model should simulate the current velocity by considering the effects of velocity, depth of flow, and type of vegetation along the canal. Total of 48 models have been simulated to investigate the effect of roughness in the canal. The results indicated that, by enhancing the velocity, the effect of vegetation in decreasing the bed velocity is negligible, while when the current has lower speed, the effect of vegetation on decreasing the bed velocity is obviously considerable.

1. Introduction

Considering the impact of each variable is a very popular field within the analytical and statistical methods and intelligent systems [114]. This can help research for better modeling considering the relation of variables or interaction of them toward reaching a better condition for the objective function in control and engineering [1527]. Consequently, it is necessary to study the effects of the passive factors on the active domain [2836]. Because of the effect of vegetation on reducing the discharge capacity of rivers [37], pruning plants was necessary to improve the condition of rivers. One of the important effects of vegetation in river protection is the action of roots, which cause soil consolidation and soil structure improvement and, by enhancing the shear strength of soil, increase the resistance of canal walls against the erosive force of water. The outer limbs of the plant increase the roughness of the canal walls and reduce the flow velocity and deplete the flow energy in vicinity of the walls. Vegetation by reducing the shear stress of the canal bed reduces flood discharge and sedimentation in the intervals between vegetation and increases the stability of the walls [3841].

One of the main factors influencing the speed, depth, and extent of flood in this method is Manning’s roughness coefficient. On the other hand, soil cover [42], especially vegetation, is one of the most determining factors in Manning’s roughness coefficient. Therefore, it is expected that those seasonal changes in the vegetation of the region will play an important role in the calculated value of Manning’s roughness coefficient and ultimately in predicting the flood wave behavior [4345]. The roughness caused by plants’ resistance to flood current depends on the flow and plant conditions. Flow conditions include depth and velocity of the plant, and plant conditions include plant type, hardness or flexibility, dimensions, density, and shape of the plant [46]. In general, the issue discussed in this research is the optimization of flood-induced flow in canals by considering the effect of vegetation-induced roughness. Therefore, the effect of plants on the roughness coefficient and canal transmission coefficient and in consequence the flow depth should be evaluated [4748].

Current resistance is generally known by its roughness coefficient. The equation that is mainly used in this field is Manning equation. The ratio of shear velocity to average current velocity  is another form of current resistance. The reason for using the  ratio is that it is dimensionless and has a strong theoretical basis. The reason for using Manning roughness coefficient is its pervasiveness. According to Freeman et al. [49], the Manning roughness coefficient for plants was calculated according to the Kouwen and Unny [50] method for incremental resistance. This method involves increasing the roughness for various surface and plant irregularities. Manning’s roughness coefficient has all the factors affecting the resistance of the canal. Therefore, the appropriate way to more accurately estimate this coefficient is to know the factors affecting this coefficient [51].

To calculate the flow rate, velocity, and depth of flow in canals as well as flood and sediment estimation, it is important to evaluate the flow resistance. To determine the flow resistance in open ducts, Manning, Chézy, and Darcy–Weisbach relations are used [52]. In these relations, there are parameters such as Manning’s roughness coefficient (n), Chézy roughness coefficient (C), and Darcy–Weisbach coefficient (f). All three of these coefficients are a kind of flow resistance coefficient that is widely used in the equations governing flow in rivers [53].

The three relations that express the relationship between the average flow velocity (V) and the resistance and geometric and hydraulic coefficients of the canal are as follows:where nf, and c are Manning, Darcy–Weisbach, and Chézy coefficients, respectively. V = average flow velocity, R = hydraulic radius, Sf = slope of energy line, which in uniform flow is equal to the slope of the canal bed,  = gravitational acceleration, and Kn is a coefficient whose value is equal to 1 in the SI system and 1.486 in the English system. The coefficients of resistance in equations (1) to (3) are related as follows:

Based on the boundary layer theory, the flow resistance for rough substrates is determined from the following general relation:where f = Darcy–Weisbach coefficient of friction, y = flow depth, Ks = bed roughness size, and A = constant coefficient.

On the other hand, the relationship between the Darcy–Weisbach coefficient of friction and the shear velocity of the flow is as follows:

By using equation (6), equation (5) is converted as follows:

Investigation on the effect of vegetation arrangement on shear velocity of flow in laboratory conditions showed that, with increasing the shear Reynolds number (), the numerical value of the  ratio also increases; in other words the amount of roughness coefficient increases with a slight difference in the cases without vegetation, checkered arrangement, and cross arrangement, respectively [54].

Roughness in river vegetation is simulated in mathematical models with a variable floor slope flume by different densities and discharges. The vegetation considered submerged in the bed of the flume. Results showed that, with increasing vegetation density, canal roughness and flow shear speed increase and with increasing flow rate and depth, Manning’s roughness coefficient decreases. Factors affecting the roughness caused by vegetation include the effect of plant density and arrangement on flow resistance, the effect of flow velocity on flow resistance, and the effect of depth [4555].

One of the works that has been done on the effect of vegetation on the roughness coefficient is Darby [56] study, which investigates a flood wave model that considers all the effects of vegetation on the roughness coefficient. There are currently two methods for estimating vegetation roughness. One method is to add the thrust force effect to Manning’s equation [475758] and the other method is to increase the canal bed roughness (Manning-Strickler coefficient) [455961]. These two methods provide acceptable results in models designed to simulate floodplain flow. Wang et al. [62] simulate the floodplain with submerged vegetation using these two methods and to increase the accuracy of the results, they suggested using the effective height of the plant under running water instead of using the actual height of the plant. Freeman et al. [49] provided equations for determining the coefficient of vegetation roughness under different conditions. Lee et al. [63] proposed a method for calculating the Manning coefficient using the flow velocity ratio at different depths. Much research has been done on the Manning roughness coefficient in rivers, and researchers [496366] sought to obtain a specific number for n to use in river engineering. However, since the depth and geometric conditions of rivers are completely variable in different places, the values of Manning roughness coefficient have changed subsequently, and it has not been possible to choose a fixed number. In river engineering software, the Manning roughness coefficient is determined only for specific and constant conditions or normal flow. Lee et al. [63] stated that seasonal conditions, density, and type of vegetation should also be considered. Hydraulic roughness and Manning roughness coefficient n of the plant were obtained by estimating the total Manning roughness coefficient from the matching of the measured water surface curve and water surface height. The following equation is used for the flow surface curve:where  is the depth of water change, S0 is the slope of the canal floor, Sf is the slope of the energy line, and Fr is the Froude number which is obtained from the following equation:where D is the characteristic length of the canal. Flood flow velocity is one of the important parameters of flood waves, which is very important in calculating the water level profile and energy consumption. In the cases where there are many limitations for researchers due to the wide range of experimental dimensions and the variety of design parameters, the use of numerical methods that are able to estimate the rest of the unknown results with acceptable accuracy is economically justified.

FLOW-3D software uses Finite Difference Method (FDM) for numerical solution of two-dimensional and three-dimensional flow. This software is dedicated to computational fluid dynamics (CFD) and is provided by Flow Science [67]. The flow is divided into networks with tubular cells. For each cell there are values of dependent variables and all variables are calculated in the center of the cell, except for the velocity, which is calculated at the center of the cell. In this software, two numerical techniques have been used for geometric simulation, FAVOR™ (Fractional-Area-Volume-Obstacle-Representation) and the VOF (Volume-of-Fluid) method. The equations used at this model for this research include the principle of mass survival and the magnitude of motion as follows. The fluid motion equations in three dimensions, including the Navier–Stokes equations with some additional terms, are as follows:where  are mass accelerations in the directions xyz and  are viscosity accelerations in the directions xyz and are obtained from the following equations:

Shear stresses  in equation (11) are obtained from the following equations:

The standard model is used for high Reynolds currents, but in this model, RNG theory allows the analytical differential formula to be used for the effective viscosity that occurs at low Reynolds numbers. Therefore, the RNG model can be used for low and high Reynolds currents.

Weather changes are high and this affects many factors continuously. The presence of vegetation in any area reduces the velocity of surface flows and prevents soil erosion, so vegetation will have a significant impact on reducing destructive floods. One of the methods of erosion protection in floodplain watersheds is the use of biological methods. The presence of vegetation in watersheds reduces the flow rate during floods and prevents soil erosion. The external organs of plants increase the roughness and decrease the velocity of water flow and thus reduce its shear stress energy. One of the important factors with which the hydraulic resistance of plants is expressed is the roughness coefficient. Measuring the roughness coefficient of plants and investigating their effect on reducing velocity and shear stress of flow is of special importance.

Roughness coefficients in canals are affected by two main factors, namely, flow conditions and vegetation characteristics [68]. So far, much research has been done on the effect of the roughness factor created by vegetation, but the issue of plant density has received less attention. For this purpose, this study was conducted to investigate the effect of vegetation density on flow velocity changes.

In a study conducted using a software model on three density modes in the submerged state effect on flow velocity changes in 48 different modes was investigated (Table 1).

Table 1 

The studied models.

The number of cells used in this simulation is equal to 1955888 cells. The boundary conditions were introduced to the model as a constant speed and depth (Figure 1). At the output boundary, due to the presence of supercritical current, no parameter for the current is considered. Absolute roughness for floors and walls was introduced to the model (Figure 1). In this case, the flow was assumed to be nonviscous and air entry into the flow was not considered. After  seconds, this model reached a convergence accuracy of .

Figure 1 

The simulated model and its boundary conditions.

Due to the fact that it is not possible to model the vegetation in FLOW-3D software, in this research, the vegetation of small soft plants was studied so that Manning’s coefficients can be entered into the canal bed in the form of roughness coefficients obtained from the studies of Chow [69] in similar conditions. In practice, in such modeling, the effect of plant height is eliminated due to the small height of herbaceous plants, and modeling can provide relatively acceptable results in these conditions.

48 models with input velocities proportional to the height of the regular semihexagonal canal were considered to create supercritical conditions. Manning coefficients were applied based on Chow [69] studies in order to control the canal bed. Speed profiles were drawn and discussed.

Any control and simulation system has some inputs that we should determine to test any technology [7077]. Determination and true implementation of such parameters is one of the key steps of any simulation [237881] and computing procedure [8286]. The input current is created by applying the flow rate through the VFR (Volume Flow Rate) option and the output flow is considered Output and for other borders the Symmetry option is considered.

Simulation of the models and checking their action and responses and observing how a process behaves is one of the accepted methods in engineering and science [8788]. For verification of FLOW-3D software, the results of computer simulations are compared with laboratory measurements and according to the values of computational error, convergence error, and the time required for convergence, the most appropriate option for real-time simulation is selected (Figures 2 and 3 ).

Figure 2 

Modeling the plant with cylindrical tubes at the bottom of the canal.

Figure 3 

Velocity profiles in positions 2 and 5.

The canal is 7 meters long, 0.5 meters wide, and 0.8 meters deep. This test was used to validate the application of the software to predict the flow rate parameters. In this experiment, instead of using the plant, cylindrical pipes were used in the bottom of the canal.

The conditions of this modeling are similar to the laboratory conditions and the boundary conditions used in the laboratory were used for numerical modeling. The critical flow enters the simulation model from the upstream boundary, so in the upstream boundary conditions, critical velocity and depth are considered. The flow at the downstream boundary is supercritical, so no parameters are applied to the downstream boundary.

The software well predicts the process of changing the speed profile in the open canal along with the considered obstacles. The error in the calculated speed values can be due to the complexity of the flow and the interaction of the turbulence caused by the roughness of the floor with the turbulence caused by the three-dimensional cycles in the hydraulic jump. As a result, the software is able to predict the speed distribution in open canals.

2. Modeling Results

After analyzing the models, the results were shown in graphs (Figures 414 ). The total number of experiments in this study was 48 due to the limitations of modeling.


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Figure 4 

Flow velocity profiles for canals with a depth of 1 m and flow velocities of 3–3.3 m/s. Canal with a depth of 1 meter and a flow velocity of (a) 3 meters per second, (b) 3.1 meters per second, (c) 3.2 meters per second, and (d) 3.3 meters per second.

Figure 5 

Canal diagram with a depth of 1 meter and a flow rate of 3 meters per second.

Figure 6 

Canal diagram with a depth of 1 meter and a flow rate of 3.1 meters per second.

Figure 7 

Canal diagram with a depth of 1 meter and a flow rate of 3.2 meters per second.

Figure 8 

Canal diagram with a depth of 1 meter and a flow rate of 3.3 meters per second.


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Figure 9 

Flow velocity profiles for canals with a depth of 2 m and flow velocities of 4–4.3 m/s. Canal with a depth of 2 meters and a flow rate of (a) 4 meters per second, (b) 4.1 meters per second, (c) 4.2 meters per second, and (d) 4.3 meters per second.

Figure 10 

Canal diagram with a depth of 2 meters and a flow rate of 4 meters per second.

Figure 11 

Canal diagram with a depth of 2 meters and a flow rate of 4.1 meters per second.

Figure 12 

Canal diagram with a depth of 2 meters and a flow rate of 4.2 meters per second.

Figure 13 

Canal diagram with a depth of 2 meters and a flow rate of 4.3 meters per second.


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Figure 14 

Flow velocity profiles for canals with a depth of 3 m and flow velocities of 5–5.3 m/s. Canal with a depth of 2 meters and a flow rate of (a) 4 meters per second, (b) 4.1 meters per second, (c) 4.2 meters per second, and (d) 4.3 meters per second.

To investigate the effects of roughness with flow velocity, the trend of flow velocity changes at different depths and with supercritical flow to a Froude number proportional to the depth of the section has been obtained.

According to the velocity profiles of Figure 5, it can be seen that, with the increasing of Manning’s coefficient, the canal bed speed decreases.

According to Figures 5 to 8, it can be found that, with increasing the Manning’s coefficient, the canal bed speed decreases. But this deceleration is more noticeable than the deceleration of the models 1 to 12, which can be justified by increasing the speed and of course increasing the Froude number.

According to Figure 10, we see that, with increasing Manning’s coefficient, the canal bed speed decreases.

According to Figure 11, we see that, with increasing Manning’s coefficient, the canal bed speed decreases. But this deceleration is more noticeable than the deceleration of Figures 510, which can be justified by increasing the speed and, of course, increasing the Froude number.

With increasing Manning’s coefficient, the canal bed speed decreases (Figure 12). But this deceleration is more noticeable than the deceleration of the higher models (Figures 58 and 1011), which can be justified by increasing the speed and, of course, increasing the Froude number.

According to Figure 13, with increasing Manning’s coefficient, the canal bed speed decreases. But this deceleration is more noticeable than the deceleration of Figures 5 to 12, which can be justified by increasing the speed and, of course, increasing the Froude number.

According to Figure 15, with increasing Manning’s coefficient, the canal bed speed decreases.

Figure 15 

Canal diagram with a depth of 3 meters and a flow rate of 5 meters per second.

According to Figure 16, with increasing Manning’s coefficient, the canal bed speed decreases. But this deceleration is more noticeable than the deceleration of the higher model, which can be justified by increasing the speed and, of course, increasing the Froude number.

Figure 16 

Canal diagram with a depth of 3 meters and a flow rate of 5.1 meters per second.

According to Figure 17, it is clear that, with increasing Manning’s coefficient, the canal bed speed decreases. But this deceleration is more noticeable than the deceleration of the higher models, which can be justified by increasing the speed and, of course, increasing the Froude number.

Figure 17 

Canal diagram with a depth of 3 meters and a flow rate of 5.2 meters per second.

According to Figure 18, with increasing Manning’s coefficient, the canal bed speed decreases. But this deceleration is more noticeable than the deceleration of the higher models, which can be justified by increasing the speed and, of course, increasing the Froude number.

Figure 18 

Canal diagram with a depth of 3 meters and a flow rate of 5.3 meters per second.

According to Figure 19, it can be seen that the vegetation placed in front of the flow input velocity has negligible effect on the reduction of velocity, which of course can be justified due to the flexibility of the vegetation. The only unusual thing is the unexpected decrease in floor speed of 3 m/s compared to higher speeds.


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Figure 19 

Comparison of velocity profiles with the same plant densities (depth 1 m). Comparison of velocity profiles with (a) plant densities of 25%, depth 1 m; (b) plant densities of 50%, depth 1 m; and (c) plant densities of 75%, depth 1 m.

According to Figure 20, by increasing the speed of vegetation, the effect of vegetation on reducing the flow rate becomes more noticeable. And the role of input current does not have much effect in reducing speed.


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Figure 20 

Comparison of velocity profiles with the same plant densities (depth 2 m). Comparison of velocity profiles with (a) plant densities of 25%, depth 2 m; (b) plant densities of 50%, depth 2 m; and (c) plant densities of 75%, depth 2 m.

According to Figure 21, it can be seen that, with increasing speed, the effect of vegetation on reducing the bed flow rate becomes more noticeable and the role of the input current does not have much effect. In general, it can be seen that, by increasing the speed of the input current, the slope of the profiles increases from the bed to the water surface and due to the fact that, in software, the roughness coefficient applies to the channel floor only in the boundary conditions, this can be perfectly justified. Of course, it can be noted that, due to the flexible conditions of the vegetation of the bed, this modeling can show acceptable results for such grasses in the canal floor. In the next directions, we may try application of swarm-based optimization methods for modeling and finding the most effective factors in this research [27815188994]. In future, we can also apply the simulation logic and software of this research for other domains such as power engineering [9599].


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Figure 21 

Comparison of velocity profiles with the same plant densities (depth 3 m). Comparison of velocity profiles with (a) plant densities of 25%, depth 3 m; (b) plant densities of 50%, depth 3 m; and (c) plant densities of 75%, depth 3 m.

3. Conclusion

The effects of vegetation on the flood canal were investigated by numerical modeling with FLOW-3D software. After analyzing the results, the following conclusions were reached:(i)Increasing the density of vegetation reduces the velocity of the canal floor but has no effect on the velocity of the canal surface.(ii)Increasing the Froude number is directly related to increasing the speed of the canal floor.(iii)In the canal with a depth of one meter, a sudden increase in speed can be observed from the lowest speed and higher speed, which is justified by the sudden increase in Froude number.(iv)As the inlet flow rate increases, the slope of the profiles from the bed to the water surface increases.(v)By reducing the Froude number, the effect of vegetation on reducing the flow bed rate becomes more noticeable. And the input velocity in reducing the velocity of the canal floor does not have much effect.(vi)At a flow rate between 3 and 3.3 meters per second due to the shallow depth of the canal and the higher landing number a more critical area is observed in which the flow bed velocity in this area is between 2.86 and 3.1 m/s.(vii)Due to the critical flow velocity and the slight effect of the roughness of the horseshoe vortex floor, it is not visible and is only partially observed in models 1-2-3 and 21.(viii)As the flow rate increases, the effect of vegetation on the rate of bed reduction decreases.(ix)In conditions where less current intensity is passing, vegetation has a greater effect on reducing current intensity and energy consumption increases.(x)In the case of using the flow rate of 0.8 cubic meters per second, the velocity distribution and flow regime show about 20% more energy consumption than in the case of using the flow rate of 1.3 cubic meters per second.

Nomenclature

n:Manning’s roughness coefficient
C:Chézy roughness coefficient
f:Darcy–Weisbach coefficient
V:Flow velocity
R:Hydraulic radius
g:Gravitational acceleration
y:Flow depth
Ks:Bed roughness
A:Constant coefficient
:Reynolds number
y/∂x:Depth of water change
S0:Slope of the canal floor
Sf:Slope of energy line
Fr:Froude number
D:Characteristic length of the canal
G:Mass acceleration
:Shear stresses.

Data Availability

All data are included within the paper.

Conflicts of Interest

The authors declare that they have no conflicts of interest.

Acknowledgments

This work was partially supported by the National Natural Science Foundation of China under Contract no. 71761030 and Natural Science Foundation of Inner Mongolia under Contract no. 2019LH07003.

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Strain rate magnitude at the free surface, illustrating Kelvin-Helmoltz (KH) shear instabilities.

On the reef scale hydrodynamics at Sodwana Bay, South Africa

Environmental Fluid Mechanics (2022)Cite this article

Abstract

The hydrodynamics of coral reefs strongly influences their biological functioning, impacting processes such as nutrient availability and uptake, recruitment success and bleaching. For example, coral reefs located in oligotrophic regions depend on upwelling for nutrient supply. Coral reefs at Sodwana Bay, located on the east coast of South Africa, are an example of high latitude marginal reefs. These reefs are subjected to complex hydrodynamic forcings due to the interaction between the strong Agulhas current and the highly variable topography of the region. In this study, we explore the reef scale hydrodynamics resulting from the bathymetry for two steady current scenarios at Two-Mile Reef (TMR) using a combination of field data and numerical simulations. The influence of tides or waves was not considered for this study as well as reef-scale roughness. Tilt current meters with onboard temperature sensors were deployed at selected locations within TMR. We used field observations to identify the dominant flow conditions on the reef for numerical simulations that focused on the hydrodynamics driven by mean currents. During the field campaign, southerly currents were the predominant flow feature with occasional flow reversals to the north. Northerly currents were associated with greater variability towards the southern end of TMR. Numerical simulations showed that Jesser Point was central to the development of flow features for both the northerly and southerly current scenarios. High current variability in the south of TMR during reverse currents is related to the formation of Kelvin-Helmholtz type shear instabilities along the outer edge of an eddy formed north of Jesser Point. Furthermore, downward vertical velocities were computed along the offshore shelf at TMR during southerly currents. Current reversals caused a change in vertical velocities to an upward direction due to the orientation of the bathymetry relative to flow directions.

Highlights

  • A predominant southerly current was measured at Two-Mile Reef with occasional reversals towards the north.
  • Field observations indicated that northerly currents are spatially varied along Two-Mile Reef.
  • Simulation of reverse currents show the formation of a separated flow due to interaction with Jesser Point with Kelvin–Helmholtz type shear instabilities along the seaward edge.

지금까지 Sodwana Bay에서 자세한 암초 규모 유체 역학을 모델링하려는 시도는 없었습니다. 이러한 모델의 결과는 규모가 있는 산호초 사이의 흐름이 산호초 건강에 어떤 영향을 미치는지 탐색하는 데 사용할 수 있습니다. 이 연구에서는 Sodwana Bay의 유체역학을 탐색하는 데 사용할 수 있는 LES 모델을 개발하기 위한 단계별 접근 방식을 구현합니다. 여기서 우리는 이 초기 단계에서 파도와 조수의 영향을 배제하면서 Agulhas 해류의 유체역학에 초점을 맞춥니다. 이 접근법은 흐름의 첫 번째 LES를 제시하고 Sodwana Bay의 산호초에서 혼합함으로써 향후 연구의 기초를 제공합니다.

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Figure 2: 3D (left) and 2D (right) views of wave elevation using case C

CFD 접근법을 사용하여 파도에서 하이드로포일의 SEAKEEPING 성능

SYAFIQ ZIKRYAND FITRIADHY*
Faculty of Ocean Engineering Technology and Informatics, Universiti Malaysia Terengganu, 21030 Kuala
Terengganu, Terengganu, Malaysia
*
Corresponding author: naoe.afit@gmail.com http://doi.org/10.46754/umtjur.2021.07.017

Abstract

수중익선은 일반적으로 열악한 환경 조건으로 인해 승객의 편안함에 영향을 미칠 수 있는 높은 저항과 과도한 수직 운동(히브 및 피치)을 경험합니다. 따라서 복잡한 유체역학적 현상이 존재하기 때문에 파랑에서 수중익선의 내항성능을 규명할 필요가 있다.

이를 위해 수중익선 운동에 대한 CFD(Computational Fluid Dynamic) 해석을 제안한다. Froude Number 및 포일 받음각과 같은 여러 매개변수가 고려되었습니다.

그 결과 Froude Number의 후속 증가는 히브 및 피치 운동에 반비례한다는 것이 밝혀졌습니다. 본질적으로 이것은 높은 응답 진폭 연산자(RAO)의 형태로 제공되는 수중익선 항해 성능의 업그레이드로 이어졌습니다.

또한 포일 선수의 증가하는 각도는 히브 운동에 비례하는 반면, 포일 선미는 7.5o에서 낮은 히브 운동을 보였고, 그 다음으로 5o, 10o 순으로 나타났다. 피치모션의 경우 포일 보우의 증가는 5o에서 더 낮았고, 그 다음이 10o, 7.5o 순이었다. 포일 선미의 증가는 수중익선에 의한 피치 모션 경험에 비례했습니다.

일반적으로 이 CFD 시뮬레이션은 앞서 언급한 설계 매개변수와 관련하여 공해 상태에서 수중익선 설계의 운영 효율성을 보장하는 데 매우 유용합니다.

Keywords

CFD, hydrofoil, foil angle of attack, heave, pitch.

Figure 1: Overall mesh block being used in simulation
Figure 1: Overall mesh block being used in simulation
Figure 2: 3D (left) and 2D (right) views of wave elevation using case C
Figure 2: 3D (left) and 2D (right) views of wave elevation using case C

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