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Unsteady Cavitating Flow around a Hydrofoil Simulated Using the Partially-Averaged Navier-Stokes Model 被引量:6

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摘要 Numerical simulations of unsteady cavitating flow around a NACA66-mod hydrofoil were performed using the partially-averaged Navier-Stokes method with different values of the resolution control parameters (f k =1.0-0.2,fε =1).With decreasing fk,the predicted cavitating flow becomes unsteady as the time-averaged turbulent viscosity at the rear part of the attached cavity is gradually reduced.For fk =0.9 and 0.8,the cavity becomes unstable and its length dramatically expands and shrinks,but the calculation fails to predict the vapor cloud shedding behavior observed experimentally.With smaller fk less than 0.7,the cloud shedding behavior is simulated numerically and the predicted cavity shedding frequency increases.With fk =0.2,the whole cavitating flow evolution can be reasonably reproduced including the cavity growth/destabilization observed previously.The reentrant flow along the suction surface of the hydrofoil is the main trigger to cause the vapor cloud shedding.The wall pressure along the hydrofoil surface oscillates greatly due to the dynamic cavity shedding.Comparing the simulations and experiments,it is confirmed that for the PANS method,resolution control parameters of fk =0.2and fε =1 are recommended for numerical simulations of unsteady cavitating flows.Thus,the present study shows that the PANS method is an effective approach for predicting unsteady cavitating flow over hydrofoils.
作者 季斌 罗先武 吴玉林 许洪元 JI Bin;LUO Xian-Wu;WU Yu-Lin;XU Hong-Yuan(State Key Laboratory of Hydroscience and Engineering,Tsinghua University,Beijing 100084)
出处 《Chinese Physics Letters》 SCIE CAS CSCD 2012年第7期198-202,共5页 中国物理快报(英文版)
基金 Supported by the National Natural Science Fund of China under Grant Nos 51179091 and 50976061, the Major NationalScientific Instrument and Equipment Development Project (No 2011YQ07004901), and the China Postdoctoral Science Foundation(No 2011M500314).
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