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+//consider the CJ-1 at sea level.
+b=16.25;//wingspan(meter)
+S=29.54;//wingarea(m^2)
+AR=b^2/S;//aspect ratio
+D=1.225;//density at sea level(Kg/m^3)
+W=88176.75;//normal gross weight(N)
+Tf=2*16245//thrust (N) provided by two turbofan engine
+Cdo=0.02;//parasite drag coefficient
+e=0.81;//oswald efficiency factor
+V=linspace(40,300,500);//velocity over which we have to find thrust(40 to 300 m/s and over 500 points)