Numerical Investigation on Vortex Shedding from a Hydrofoil with a Beveled Trailing Edge

To better understand the vortex shedding mechanism and to assess the capability of our numerical methodology, we conducted numerical investigations of vortex shedding from truncated and oblique trailing edges of a modified NACA 0009 hydrofoil. The hybrid particle-mesh method and the vorticity-based...

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Bibliographic Details
Main Authors: Seung-Jae Lee, Jun-Hyeok Lee, Jung-Chun Suh
Format: Article
Language:English
Published: Wiley 2015-01-01
Series:Modelling and Simulation in Engineering
Online Access:http://dx.doi.org/10.1155/2015/565417
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Summary:To better understand the vortex shedding mechanism and to assess the capability of our numerical methodology, we conducted numerical investigations of vortex shedding from truncated and oblique trailing edges of a modified NACA 0009 hydrofoil. The hybrid particle-mesh method and the vorticity-based subgrid scale model were employed to simulate these turbulent wake flows. The hybrid particle-mesh method combines the vortex-in-cell and the penalization methods. We have implemented numerical schemes to more efficiently use available computational resources. In this study, we numerically investigated vortex shedding from various beveled trailing edges at a Reynolds number of 106. We then compared the numerical results with the experimental data, which show good agreement. We also conducted numerical simulations of wakes behind the hydrofoil at rest in periodically varying flows. Results reveal that vortex shedding is affected by the periodicity of a free-stream flow, as well as the trailing-edge shape.
ISSN:1687-5591
1687-5605