Parallel Simulation of the Aerodynamic Characteristics of a Blunt Cone in Multiple Flow Regimes

Author:

Jiang Dingwu1,Li Jin1,Wang Pei1,Mao Meiliang1

Affiliation:

1. Computational Aerodynamics Institute, China Aerodynamics Research and Development Center, China

Funder

NNW

NSFC

Publisher

ACM

Reference50 articles.

1. Ivanov MS , Gimelshein SF. 1998 . Computational hypersonic rarefied flows . Annual Review of Fluid Mechanics , 1998,30: 469 - 505 . Ivanov MS, Gimelshein SF. 1998. Computational hypersonic rarefied flows. Annual Review of Fluid Mechanics, 1998,30: 469-505.

2. Bird GA. 1963. Approach to translational equilibrium in a rigid sphere gas . Physics of Fluids , 1963 ,6(10): 1518 - 1519 . Bird GA.1963. Approach to translational equilibrium in a rigid sphere gas. Physics of Fluids, 1963,6(10): 1518-1519.

3. Pulvirenti M , Wagner W , Rossi MBZ . 1994 . Convergence of particle schemes for the Boltzmann-equation . European Journal of Mechanics B-Fluids , 1994,13(3): 339 - 351 . Pulvirenti M, Wagner W, Rossi MBZ. 1994. Convergence of particle schemes for the Boltzmann-equation. European Journal of Mechanics B-Fluids, 1994,13(3): 339-351.

4. Wagner W. 1992 . A convergence proof for Bird's direct simulation Monte Carlo method for the Boltzmann equation . Journal of Statistical Physics , 1992,66(3-4): 1011 - 1044 . Wagner W. 1992. A convergence proof for Bird's direct simulation Monte Carlo method for the Boltzmann equation. Journal of Statistical Physics, 1992,66(3-4): 1011-1044.

5. Candler GV Boyd ID Levin DA. 1993. Continuum and DSMC Analysis of Bow Shock Flight Experiments. AIAA paper 93-0275. Candler GV Boyd ID Levin DA. 1993. Continuum and DSMC Analysis of Bow Shock Flight Experiments. AIAA paper 93-0275.

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