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。
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。
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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