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panair
- 亚声速超声速高阶空气动力学板块代码。所有线化理论板块方法中最可信和准确的。-High order aerodynamic panel code. The most versatile and accurate of all the linear theory panel codes. Subsonic/supersonic solutions with linear source strength variation and quadratic doublet strength variatio
Shock-Wave-Calculation
- 用CFD方法计算超声速下小攻角翼型产生的激波-CFD method with a small angle of attack under supersonic shock wave generated airfoil
Prandtl_Meyer_expansion_wave
- 《计算流体力学及其应用》chapter8 二维超声速流动的数值解——普朗特—迈耶稀疏波的程序。Fortran编写。-A Fortran program of Prandtl-Meyer expansion wave in two-dimensional supersonic flow. Based on John D. Anderson, JR., Chapter 8, In Computational Fluid Dynamics
CFD-John-D.Anderson-第10章
- John-D.Anderson的计算流体力学基础及应用第10章超声速外略平板的程序，之前传过一份，有一些问题，之后从这个网站上看到过几个例子，学习了下，现在通过学习改好了，请大家指点，谢谢！(Computational fluid mechanics foundation and application of the tenth chapter of supersonic John-D.Anderson slightly outside the plate before a procedure,
Moc.java
- NASA的喷管设计程序，采用特征线方法，JAVA设计语言。(A Java Application to perform two dimensional analysis of supersonic flow through nozzles using the method of characteristics.)