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+b=12.29;//wing span in meter
+S=23.69;//wing area in m^2
+AR=b^2/S //aspect ratio
+D=1.225;//density at standard sea level,Kg/m^3
+V=48.3*5/18 //velocity of flyer(m/s)
+e=0.93;//span efficiency factor
+W=3337.5;//total weight of the flyer in newton
+L=W/2;//lift on one wing(out of two)in newton
+q=(D*V^2/2) //dynamic pressure(N/m^2)
+Cl=L/(q*S)//lift coefficient
+Cdi=Cl^2/(%pi*e*AR) //induced drag coefficient \ No newline at end of file