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 Description: Using oblique shock- expansion wave theory rhombus symmetrical airfoil flow field in each surface pressure coefficient and airfoil lift and drag coefficients
 Downloaders recently: [More information of uploader 贾雷明]
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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
    

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