Numerical results are obtained for the three dimensional compressible flow field of low pressure turbine exhaust hood.

以数值模拟为手段，描述了透平低压排气缸内部复杂的三维可压缩湍流流场。

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In this way, parameters distribution of two dimensional compressible (Plane and axisymmetric) turbulent jets mixing flow field can be calculated.

用这种方法可以计算等截面和变截面二维(平面的和轴对称的)可压缩紊流射流掺混的流场分布。

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United flow field at all flow speeds in the chamber and nozzle of SRM is solved by using the compressible form of the SIMPLE algorithm.

采用SIMPL E算法的可压缩形式求解固体火箭发动机燃烧室喷管内的全速度统一流场；

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