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//Wing area(in ft^2):
A=1600;
//Aspect ratio:
ar=6.5;
//Groos weight of aircraft(in lbf):
W=150000;
//Coefficient of drag at zero lift :
Cd0=0.0182;
//Sonic speed at sea level(in mph):
c=759;
//Density of air(in slug/ft^3):
p=0.00238;
//Srall speed at sea level(in mph):
Vssl=175;
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