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Consider a generic combat aircraft of Mass =10000kg, Wing Area =38m2, Aspect Ratio = 2.0, epsilon =0.8, Cmax =1.7, CD0 = 0.02 and Thrust =80kN. Compute the following at 3 km altitude:
a. Rate of climb at 1.3 times stall velocity.
b. Rate of climb 1.2 time minimum thrust velocity.

Sagot :

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