1·A class of compressible flow Mach number limit.
一类可压缩流的马赫数极限。
2·Some cases of compressible flow as well as incompressible flow are presented.
分别对可压缩叶栅流场的亚音速和跨音速流动进行了数值模拟计算。
3·The Vortex Dynamics Equation is developed for compressible flow and its characteristics are analyzed.
推导了可压缩流动旋涡动力学基本方程，并分析了其基本性质。
4·In Chapter IV, we focused on the global existence of 2-d piston problem in isentropic compressible flow.
第四章主要研究二维等嫡可压缩流轴对称活塞问题激波解的整体存在性。
5·In the numerical simulation, a weakly compressible flow model and the body fitted grid technique are used.
在数值模拟中，采用了弱压缩流的控制方程，用贴体坐标技术进行了网格生成。
6·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。
7·An implicit time-marching method is presented for computing the three-dimensional steady inviscid compressible flow fields.
本文提出了求解三维定常无粘可压缩流场问题的一种隐式时间推进法。
8·The large eddy simulation is applied to simulate a 3-d square channel compressible flow around a wall-mounted rectangle cylinder.
该文利用大涡模拟，对可压缩流体绕经安装在方管底部的长方体和矩形体的绕流现象进行了三维数值模拟。
9·The effect of acoustic excitation on the flow asymmetry over a slender body in compressible flows was investigated in a transonic wind tunnel.
在跨声速风洞中研究了声激励对于可压缩流中细长旋成体大迎角流动非对称性的影响效果。
10·The study of the mechanism of transition of compressible flow is of significant importance both from the theoretical and practical point of view.
对可压缩流动转捩机制的研究有重要的理论与工程意义。