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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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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1721554708812791808 |