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。
2
An analysis of applicability and limitations of the method in the problems of shocklayer 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。
3
In this paper, the nonequilibrium viscous shocklayer equations have been used to calculate the hypersonic flows over blunt bodies in the fore-body region (including stagnation line and sonic line).