文件名称:source-code
介绍说明－－下载内容均来自于网络，请自行研究使用
采用斜激波-膨胀波理论计算流场中对称菱形翼型各个表面的压力系数及翼型升阻力系数-Using oblique shock- expansion wave theory rhombus symmetrical airfoil flow field in each surface pressure coefficient and airfoil lift and drag coefficients
(系统自动生成,下载前可以参看下载内容)
下载文件列表
source code\prog11\head.h
...........\......\input.dat
...........\......\main.cpp
...........\......\prog11.exe
...........\......\source.cpp
...........\.....2\head.h
...........\......\input.dat
...........\......\main.cpp
...........\......\prog12.exe
...........\......\source.cpp
...........\程序说明.pdf
...........\prog11
...........\prog12
source code