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nozzle_shock
- 喷管加激波，呵呵，大家尽快下啊下载喷管
nonconserval
- 非守恒-无激波-跨声速 非守恒-无激波-跨声速
c++编写的3阶TVD格式求解激波的程序
- 自己用c++编写的3阶TVD格式求解激波的程序，提供给大家批评指正-Their written using c++ third-order TVD scheme to solve the shock program, available to me criticism
RK
- 求解一维Euler方程，计算一维激波管问题，时间项RK，空间使用steger_warming分裂方式-Solving one-dimensional Euler equations, to calculate the one-dimensional shock tube problem, the time RK, space using two separatist
CFD_CSharp
- cfd经典问题C源代码：一维黎曼问题；一维可压N-S方程；二维斜激波刚壁反射；二维泊萧叶黏性流动；有限体积法求解库塔流-Riemann problem a compressible N-S equations of two-dimensional oblique shock wave reflection stiffness 2D Poiseuille viscous flow finite volume method to solve the Kuta flow
CFD_CSharp
- cfd经典问题C源代码：一维黎曼问题；一维可压N-S方程；二维斜激波刚壁反射；二维泊萧叶黏性流动；有限体积法求解库塔流-Riemann problem a compressible N-S equations of two-dimensional oblique shock wave reflection stiffness 2D Poiseuille viscous flow finite volume method to solve the Kuta flow
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
lax
- 使用lax差分格式计算流体力学中一维激波管问题-Computational fluid dynamics in one-dimensional shock tube problem using lax difference scheme
Appendix-C-dimensional-oblique
- 二维斜激波反射含c和Fortran源代码-Appendix C-dimensional oblique
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
Lax_Matlab(octave)
- 一维激波管matlab源程序，采用CFD数值模拟的方法，对N-S方程进行差分，获得流体解析解。-One-dimensional shock tube matlab source code, the use of CFD numerical simulation method, the NS differential equations, fluid obtained analytical solution.
A
- 一维 问题，即激波管问题，是一个典型的一维可压缩无黏气体动力学问题，并有 解析解。对它采用二阶精度 两步差分格式进行数值求解。-A one-dimensional problem that the shock tube problem is a typical one-dimensional inviscid compressible gas dynamics, and analytical solutions. It uses a two-step second order accuracy
精确解
- F语言编程解决一维激波管问题，本程序为精确解。(One dimensional shock tube problem in F programming)
Roe
- Fortran语言解决一维激波管问题，本程序为一阶迎风Roe格式(Fortran language to solve one-dimensional shock tube problem, this program is the first order upwind Roe format)
两步wendroff求解一维激波管问题
- 用C++编写程序，采用两步wendroff法，求解一维激波管问题的源码。