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姜宝森,张亮,苏鹏辉,李俊红.超声速流动中非线性EASM湍流模式应用研究
Study on the application of nonlinear EASM turbulence model in supersonic flows[J].计算力学学报,2018,35(1):117~122
超声速流动中非线性EASM湍流模式应用研究
Study on the application of nonlinear EASM turbulence model in supersonic flows
Study on the application of nonlinear EASM turbulence model in supersonic flows
投稿时间:2016-07-12  修订日期:2016-11-14
DOI:10.7511/jslx20160712002
中文关键词:  湍流模式  显示代数雷诺应力模式  可压缩修正  超声速流动  分离流动  剪切层
英文关键词:turbulence model  explicit algebraic Reynolds stress model  compressibility modification  supersonic flow  separation flow  shear layer
基金项目:
作者单位E-mail
姜宝森 中国航天空气动力技术研究院, 北京 100074  
张亮 中国航天空气动力技术研究院, 北京 100074 zinsser_1982@163.com 
苏鹏辉 中国航天空气动力技术研究院, 北京 100074  
李俊红 中国航天空气动力技术研究院, 北京 100074  
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中文摘要:
      针对超声速复杂流动区域精确模拟的需要,发展了基于k-ω可压缩修正形式的非线性显式代数雷诺应力模式(EASM),提高了该模式对超声速复杂流动的数值模拟精度。通过对二维超声速凹槽和三维双椭球的数值计算表明,与SA和SST常规线性涡黏性湍流模式比较,非线性的EASM模式对大分离以及剪切层流动结构的刻画能力更精细,对剪切层再附区的压力及摩擦系数分布模拟更加精确;EASM模式能够准确地模拟二次激波引起的压强和热流分布情况。
英文摘要:
      To meet the needs of simulating complex supersonic flow regions accurately,the nonlinear explicit algebraic Reynolds stress model (EASM) based on the form of k-ω compressibility modification is developed.The numerical simulation accuracy of the model for supersonic flow is improved.The flows of 2-D supersonic cavity and 3-D hypersonic double ellipsoid are calculated by EASM.Compared with the conventional linear eddy viscosity models(SA and SST turbulence models),EASM has the potential ability to describe the flow structure of massive separation and shear layer in more sophisticated detail and simulate pressure and friction coefficient distribution in the region where shear layer reattaches more precisely.Distribution of pressure and heat flux induced by secondary shock wave are simulated accurately.
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