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+//consider a NACA-4412 airfoil at an angle of attack of 4 degree.
+a=4;//angle of attack in degree
+//from standard table for NACA-4412 airfoil at 4 degree angle of attack we can get lift coefficient(at low speed):
+Co=0.83;//lift coefficient(at low speed)
+M=0.7;//Mach number