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机载导弹发射时燃气流场的数值模拟

姜毅,张晓琳,刘琪

JOURNAL OF PROJECTILES, ROCKETS, MISSILES AND GUIDANCE（2002）

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Abstract
采用了求解三维、非定常、雷诺平均的Navier-stokes方程的方法,对反坦克导弹的发射发动机燃气流场进行了非定常数值模拟.紊流模型为二方程模型方程,计算网格为结构化网格.计算值与试验值符合很好.
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