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Numerical Simulation for Ventilated Supercavitation High Speed Underwater Vehicle

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【作者】 杨武刚杨振才楚岩邓秋霞李亚绒张宇文

【Author】 YANG Wu-gang1,2,YANG Zhen-cai1,CHU Yan1,DENG Qiu-xia1,LI Ya-rong1,ZHANG Yu-wen2(1.Chang’an University,Xi’an 710064 Shaanxi,China;2.College of Marine,Northwestern Polytechnical University,Xi’an,710072 Shaanxi,China)

【机构】 Chang’an UniversityCollege of Marine,Northwestern Polytechnical University

【摘要】 Supercavitation is a revolutionary technique to achieve high drag reduction for underwater vehicle.It can help us to break through the conventional speed barrier.This article presents a numerical algorithm for ventilated supercavitation flow field based on mixture multiphase flow model,briefs the calculation results and compares them with that tested in high-speed water tunnel and towing tank.The mathematical model,its numerical calculation method,computational region and boundary conditions are discussed in detail.Some pertinent nondimensional parameters about the ventilated supercavitation,such as geometrical configuration of supercavity,drag coefficient and ventilation rate are investigated.Reynolds number is selected to predict gas ventilation rate instead of Froude number.Finally,based on the test and simulation results,a semi-empirical formula of the ventilation rate estimation suitable for different conical angle caritators is proposed.

【Abstract】 Supercavitation is a revolutionary technique to achieve high drag reduction for underwater vehicle.It can help us to break through the conventional speed barrier.This article presents a numerical algorithm for ventilated supercavitation flow field based on mixture multiphase flow model,briefs the calculation results and compares them with that tested in high-speed water tunnel and towing tank.The mathematical model,its numerical calculation method,computational region and boundary conditions are discussed in detail.Some pertinent nondimensional parameters about the ventilated supercavitation,such as geometrical configuration of supercavity,drag coefficient and ventilation rate are investigated.Reynolds number is selected to predict gas ventilation rate instead of Froude number.Finally,based on the test and simulation results,a semi-empirical formula of the ventilation rate estimation suitable for different conical angle caritators is proposed.

【基金】 Sponsored by National Basic Research Programof China(K1804061802)
  • 【文献出处】 Journal of China Ordnance ,兵工学报(英文版) , 编辑部邮箱 ,2009年02期
  • 【分类号】O351.3
  • 【下载频次】95
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