机械
涡度
涡流
空化
喷射(流体)
旋涡脱落
边界层
涡度方程
物理
旋涡伸展
流量(数学)
气泡
流动分离
经典力学
湍流
雷诺数
作者
Xiaojun Li,Yaoyao Liu,Zuchao Zhu,Peifeng Lin,Linmin Li
出处
期刊:Journal of Fluids Engineering-transactions of The Asme
[ASM International]
日期:2021-02-10
卷期号:143 (7)
被引量:14
摘要
Abstract The objective of this paper is to investigate the dynamic characteristics of transient cavitating flow over a twisted NACA0009 hydrofoil. The large eddy simulation (LES) approach is selected for the computation of fluid flow and the Zwart model is used for the mass transfer due to cavitation. Moreover, the skin-friction coefficient and boundary-vorticity flux (BVF) are used to study the flow separation. Numerical results show that the attached shear layer separates from the boundary layer and then squeezes to form the separation line under the obstruction of the reentrant jet. The analysis based on the terms of vorticity transport equation demonstrates that vortex stretching and vortex dilatation terms dominate the evolution of the multiscale vortex. Moreover, the secondary shedding induced by the side-entrant jet enhances the instability of partial cavities and the underlying mechanism is comprehensively revealed. Furthermore, the feature of the pressure fluctuation indicates that high pressure generated by the cavity collapse at the tail simultaneously propagates to the leading edge and downstream of the hydrofoil. This enhances the intensity of the reentrant jet and side-entrant jet, promoting occurrences of flow separation near the suction surface and cavity shedding to a certain extent.
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