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Experimental and numerical investigation of vortex dynamics in ventilated cavitating flows around a bluff body

机译:虚空体内通风空腔流动中涡流动力学的实验性和数值研究

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The objective of this paper is to investigate ventilated cavitating vortex shedding dynamics around a bluff body at Re=6.7×10~4 by experimental and numerical methods. The couple level-set and VOF (CLSVOF) method is applied to capture the air-water interface. The results show that the CLSVOF method can predict the air-water interface accurately. Two types of unsteady ventilated cavitating flows are investigated, namely vortex shedding structure (Q_v=0.174) and the Re-entrant jet (Q_v=0.31). The finite-time Lyapunov exponent (FTLE) and Lagrangian coherent structures (LCS) methods are applied to investigate the formation, evolution and shedding of ventilated cavitating vortices. For vortex shedding structure (Q_v=0.174), the vortices alternately shed from the cavity, forming the vortex street. For the re-entrant jet structures (Q_v=0.31), there exist the interaction between the vortex shedding and the re-entrant jet. The evolution of ventilated cavitation is divided into three stages: the vortex shedding, the development of re-entrant jet and the development of ventilated cavitation.
机译:本文的目的是通过实验和数值方法在重新= 6.7×10〜4处围绕凹槽体围绕凹槽体的通风空腔涡流动力学。该耦合级别和VOF(CLSVOF)方法应用于捕获空气水接口。结果表明,CLSVOF方法可以准确地预测空气界面。研究了两种类型的不稳定通风空腔流动,即涡旋脱落结构(Q_V = 0.174)和再参赛射流(Q_V = 0.31)。应用有限时间的Lyapunov指数(FTLE)和拉格朗日相干结构(LCS)方法来研究通风空腔涡旋的形成,进化和脱落。对于涡流脱落结构(Q_V = 0.174),涡流从腔中交替脱落,形成涡旋街。对于再参赛者喷射结构(Q_V = 0.31),涡旋脱落和重新参与者之间存在相互作用。通风气相的演变分为三个阶段:涡旋脱落,再参与者的开发和通风空化的发展。

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