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AUSM
- 一个矩形计算域中有一个圆形区域，圆形区域内的充满高压气体，计算域其他地方压强较低，当薄膜破裂，将会形成激波（欧拉方程编写）-A rectangular computational domain of a circular area, circular area filled with high-pressure gas within the computational domain elsewhere low pressure, when the film rupture, will form
external_compressible
- 问题考虑围绕翼型的流动在4°攻角和一个自由流马赫数0.8。流量是跨音速，并有近于上（吸气）侧中间弦m/c=0.45一个相当强烈的震撼。弦长为1米。-The problem considers the flow around an airfoil at an angle of attack and a free stream Mach number of ( ). The flow is transonic, and has a fairly stron
MacCo
- 激波管问题是一个典型的一维可压缩无黏气体动力学问题，有解析解。对它采用二阶精度两步差分格式进行数值求解。这里给出了计算程序-Shock tube problem is a typical one-dimensional compressible inviscid gas dynamics problem, there are analytical solution. It uses a two-step difference scheme of second order accuracy num
LaxWebdroff2d
- 斜激波在平面刚壁上反射问题具有解析解。对它采用具有二阶精度两步差分格式进行数值求解。这里给出了计算斜激波在平面刚壁上反射问题的计算程序。-Oblique shock wave reflection problem in the plane of the wall have just analytic solution. It uses a two-step format has second-order accuracy difference solved numerically. Here a
smcsw
- 用VB做的冲击波,使用时请小心,对机器千万损坏的请联系-Using VB to do shock wave, please be careful when using, the machine must damaged please contact