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//for the jet power executive aircraft(CJ-1):
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)
f=1119;//fuel capacity
Tf=16245;//thrust (N) provided by single turbofan engine
Sf=0.102;//specific fuel consumption(N/(hp.h))
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)
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