Chemical equilibrium is considered with the viscous shock layer equations.
采用粘性激波层控制方程和平衡化学反应气体模型。
There exists a critical state as cooling in supersonic region of shock layer.
超音速区内冷却存在临界状态。
The chemical non equilibrium viscous shock layer flows over a teflon ablative wall are calculated numerically.
本文对有泰氟隆烧蚀的化学非平衡粘性激波层流场进行了数值模拟。
An analysis of applicability and limitations of the method in the problems of shock layer stability on a flat plate are presented.
对此法用于平板上激波层稳定性问题的适用范围和限制条件作了分析。
Secondly, shock layer corrective term near the interior point in the interval is constructed via the transformation of stretched variable.
利用伸长变量，在区间内点附近构造问题解的激波层校正项；
In this paper, the nonequilibrium viscous shock layer equations have been used to calculate the hypersonic flows over blunt bodies in the fore-body region (including stagnation line and sonic line).
本文从化学非平衡粘性激波层控制方程出发，用数值法计算了高超音速钝体绕流头部区流场(包括驻点线和音速线)。
The problems of physical distortion due to the finite-difference scheme are studied in numerical solutions of the hypersonic viscous shock-layer equations.
本文讨论了高超声速粘性激波层方程数值计算时差分格式引起的物理失真问题。
The problems of physical distortion due to the finite-difference scheme are studied in numerical solutions of the hypersonic viscous shock-layer equations.
本文讨论了高超声速粘性激波层方程数值计算时差分格式引起的物理失真问题。
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