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超声速平头圆柱绕流DSMC/EPSM混合算法研究 被引量:4

The study of hybrid DSMC/EPSM method of supersonic flat-nosed cylinder
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摘要 本文将EPSM算法与DSMC方法结合 ,构造了可模拟含近连续流区及过渡流区的DSMC/EPSM混合算法。运用混合算法模拟马赫数等于 5 .37时超声速平头圆柱绕流 ,并与DSMC结果进行比较 ,证明了DSMC/EPSM混合算法的有效性 ,并对两种算法的计算效率进行了比较。 The Equilibrium Particle Simulation Method (EPSM) is combined with the direct simulation Monte Carlo (DSMC) method to produce a hybrid DSMC/EPSM method which could handle flows in the transition regime between rarefied gas flows and fully continuum flows. The supersonic flow past a flat nosed cylinder is calculated by using the DSMC method and the hybrid DSMC/EPSM method. The result of the hybrid DSMC/EPSM method is compared with the result of DSMC method to show the effectiveness of the hybrid DSMC/EPSM method.Computational efficiency of these two methods is compared.
出处 《空气动力学学报》 CSCD 北大核心 2002年第2期206-210,共5页 Acta Aerodynamica Sinica
基金 国家自然科学基金资助项目 (1 990 2 0 2 1 )
关键词 超声速平头圆柱绕流 EPSM 混合算法 衡薄气体流动 DSMC DSMC method EPSM method hybrid DSMC/EPSM method flat nosed cylinder rarefied gas dynamics
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参考文献4

  • 1[1]HASH D B,HASSAN H A, A hybrid DSMC/Navier-Stokes solver [R], AIAA Paper 95-0410,1995.
  • 2[2]BIRD G A,Near continuum impact of an under-expanded jet [C].In Proc.AIAA Computational Dynamics Conference, Page403, New York.1976.
  • 3[3]PULLIN D I,Direct simulation methods for compressible ideal gas flow [J],J.Comput.Phys.1980,34:231-244.
  • 4[4]MACROSSAN M N,Some developments of the equilibrium particle simulation method for the direct simulation of compressible flows [R],1995,NASA-CR-198175.

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