Description: 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
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File list (Check if you may need any files):
matlab-xfoil\E186.DAT
............\E186cp.txt
............\E334.dat
............\E334cp.txt
............\E637.dat
............\input-E186.dat
............\input-E334.dat
............\output-E186.dat
............\output-E334.dat
............\QUIT
............\xfoil.asv
............\xfoil.exe
............\xfoil.m
matlab-xfoil
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