This paper makes a 3-d two-phase flow united calculation of the inner flow field of chamber and nozzle in certain SRM.
对某锥柱形装药固体火箭发动机(SRM)燃烧室和喷管的内流场进行了三维两相一体化计算。
In the calculation of flow field in 2-d transonic cascade, wave has been exactly captured and results are satisfactory.
在平面叶栅跨音流场的计算中，较好地捕获了激波，与实验比较，结果令人满意。
In the calculation of flow field in 2-d transonic cascade, wave has been exactly captured and results are satisfactory.
在平面叶栅跨音流场的计算中，较好地捕获了激波，与实验比较，结果令人满意。
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