matlab-xfoil

代码说明：

  通过matlab调用xfoil程序，对翼型升阻力力矩进行计算，并将计算结果生成结果文件，程序中对三种翼型进行了计算，用户可根据需要删减或复制程序的相同部分即可(Xfoil by calling the same part of matlab procedures, the airfoil lift and drag torque is calculated, and the calculated results file is generated, the program for the three airfoils were calculated, the user can cut or copy the program as needed to)

文件列表：

matlab-xfoil
............\E186.DAT,1412,2012-05-28
............\E186cp.txt,3380,2012-05-28
............\E334.dat,1735,2012-05-28
............\E334cp.txt,3380,2012-05-28
............\E637.dat,1351,2012-05-14
............\input-E186.dat,204,2012-05-28
............\input-E334.dat,204,2012-05-28
............\output-E186.dat,1619,2012-05-28
............\output-E334.dat,1619,2012-05-28
............\htm" target=_blank>QUIT,431,2012-05-28
............\xfoil.asv,2432,2012-05-28
............\xfoil.exe,1339392,2006-05-02
............\xfoil.m,2434,2012-05-28