Numerical Simulation on Vortex Shedding from a Hydrofoil in Steady Flow

This paper presents a numerical modeling procedure for the idealization of vortex shedding effects in the wake flow field of a NACA0009 hydrofoil. During the simulation, the lift and drag acting on the hydrofoil were monitored, and the vortex-shedding frequency of the hydrofoil was analyzed. The eff...

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Main Authors: Jian Hu, Zibin Wang, Wang Zhao, Shili Sun, Cong Sun, Chunyu Guo
Format: Article
Language:English
Published: MDPI AG 2020-03-01
Series:Journal of Marine Science and Engineering
Subjects:
Online Access:https://www.mdpi.com/2077-1312/8/3/195
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spelling doaj-c04b7e57dd83408dbc3c24771714a75f2021-04-02T17:08:08ZengMDPI AGJournal of Marine Science and Engineering2077-13122020-03-018319510.3390/jmse8030195jmse8030195Numerical Simulation on Vortex Shedding from a Hydrofoil in Steady FlowJian Hu0Zibin Wang1Wang Zhao2Shili Sun3Cong Sun4Chunyu Guo5College of Shipbuilding Engineering, Harbin Engineering University, Harbin 150001, ChinaCollege of Shipbuilding Engineering, Harbin Engineering University, Harbin 150001, ChinaCollege of Shipbuilding Engineering, Harbin Engineering University, Harbin 150001, ChinaCollege of Shipbuilding Engineering, Harbin Engineering University, Harbin 150001, ChinaCollege of Shipbuilding Engineering, Harbin Engineering University, Harbin 150001, ChinaCollege of Shipbuilding Engineering, Harbin Engineering University, Harbin 150001, ChinaThis paper presents a numerical modeling procedure for the idealization of vortex shedding effects in the wake flow field of a NACA0009 hydrofoil. During the simulation, the lift and drag acting on the hydrofoil were monitored, and the vortex-shedding frequency of the hydrofoil was analyzed. The effects of inflow velocity, trailing-edge thickness, angle of attack, and maximum hydrofoil thickness on vortex shedding were investigated. The results indicate that an increase in the inflow velocity led to an increase in the vortex-shedding frequency and a negligible change in the Strouhal number. Furthermore, as the thickness of the trailing edge increased, the vortex-shedding frequency decreased gradually, whereas the Strouhal number first increased and then decreased. Vortex shedding and lift curve oscillations ceased altogether after the angle of attack of the hydrofoil increased beyond a certain threshold. When the maximum hydrofoil thickness was increased while keeping the thickness and chord length of the trailing edge constant, the vortex-shedding frequency decreased.https://www.mdpi.com/2077-1312/8/3/195vortex sheddingwakeflow-induced vibrations
collection DOAJ
language English
format Article
sources DOAJ
author Jian Hu
Zibin Wang
Wang Zhao
Shili Sun
Cong Sun
Chunyu Guo
spellingShingle Jian Hu
Zibin Wang
Wang Zhao
Shili Sun
Cong Sun
Chunyu Guo
Numerical Simulation on Vortex Shedding from a Hydrofoil in Steady Flow
Journal of Marine Science and Engineering
vortex shedding
wake
flow-induced vibrations
author_facet Jian Hu
Zibin Wang
Wang Zhao
Shili Sun
Cong Sun
Chunyu Guo
author_sort Jian Hu
title Numerical Simulation on Vortex Shedding from a Hydrofoil in Steady Flow
title_short Numerical Simulation on Vortex Shedding from a Hydrofoil in Steady Flow
title_full Numerical Simulation on Vortex Shedding from a Hydrofoil in Steady Flow
title_fullStr Numerical Simulation on Vortex Shedding from a Hydrofoil in Steady Flow
title_full_unstemmed Numerical Simulation on Vortex Shedding from a Hydrofoil in Steady Flow
title_sort numerical simulation on vortex shedding from a hydrofoil in steady flow
publisher MDPI AG
series Journal of Marine Science and Engineering
issn 2077-1312
publishDate 2020-03-01
description This paper presents a numerical modeling procedure for the idealization of vortex shedding effects in the wake flow field of a NACA0009 hydrofoil. During the simulation, the lift and drag acting on the hydrofoil were monitored, and the vortex-shedding frequency of the hydrofoil was analyzed. The effects of inflow velocity, trailing-edge thickness, angle of attack, and maximum hydrofoil thickness on vortex shedding were investigated. The results indicate that an increase in the inflow velocity led to an increase in the vortex-shedding frequency and a negligible change in the Strouhal number. Furthermore, as the thickness of the trailing edge increased, the vortex-shedding frequency decreased gradually, whereas the Strouhal number first increased and then decreased. Vortex shedding and lift curve oscillations ceased altogether after the angle of attack of the hydrofoil increased beyond a certain threshold. When the maximum hydrofoil thickness was increased while keeping the thickness and chord length of the trailing edge constant, the vortex-shedding frequency decreased.
topic vortex shedding
wake
flow-induced vibrations
url https://www.mdpi.com/2077-1312/8/3/195
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