41		=jx number of points along wing span (<202)
0.2		=omega relaxation factor
0.2		=avis viscosity coefficient
2.4             =B wing span (m)
0.291           =cxm dimensionless root chord of wing (ref.=B/2)
0.0		=dm relative camber of wing (ref.=C)
0.		=tm setting angle at root (typically zero)
0		=irect rectangular wing/elliptic (=1/0)
0.78539         =am multiplicating constant am=(wing area)/(B*C)
2.		=alphad geometric incidence (deg)
1.225		=Rho air density (kg/m**3)
13.64		=Vinf  wind velocity (m/s)
0.0000181	=Amu dynamic viscosity (kg/(m*s))