Description: 2d-airfoil-release2.0, solutions of two-dimensional wing panel method, the runtime directory in English
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2d-airfoil-release2.0
.....................\cp.dat
.....................\input.dat
.....................\main_pro.exe
.....................\plotxy.m
.....................\re-geometry.dat
.....................\使用说明--面元法解2维机翼的压力分布.txt
.....................\翼型剖面
.....................\........\na4412.dat
.....................\........\naca0010.dat
.....................\........\naca0012.dat
.....................\........\naca0021.dat
.....................\........\naca4412.dat
.....................\........\naca4420.dat
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