文件名称:source-code
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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
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下载文件列表
source code/prog11/head.h
source code/prog11/input.dat
source code/prog11/main.cpp
source code/prog11/prog11.exe
source code/prog11/source.cpp
source code/prog12/head.h
source code/prog12/input.dat
source code/prog12/main.cpp
source code/prog12/prog12.exe
source code/prog12/source.cpp
source code/程序说明.pdf
source code/prog11
source code/prog12
source code
source code/prog11/input.dat
source code/prog11/main.cpp
source code/prog11/prog11.exe
source code/prog11/source.cpp
source code/prog12/head.h
source code/prog12/input.dat
source code/prog12/main.cpp
source code/prog12/prog12.exe
source code/prog12/source.cpp
source code/程序说明.pdf
source code/prog11
source code/prog12
source code
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