9.30 A fighter jet aircraft has the following characteristics: mro 10,000 kg, S=24 m, b= 8...

 

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9.30 A fighter jet aircraft has the following characteristics: mro 10,000 kg, S=24 m, b= 8 m, T = 100 KN, e=0.8, CD = 0.015 (low subsonic), Do CDo 0.03 (transonic); Co= 0.042 (supersonic), CLmax = 1.7. a. Determine the corresponding velocity to the maximum producible load factor. b. Determine the maximum producible load factor. c. Determine the maximum producible bank angle. 9.30 A fighter jet aircraft has the following characteristics: mro 10,000 kg, S=24 m, b= 8 m, T = 100 KN, e=0.8, CD = 0.015 (low subsonic), Do CDo 0.03 (transonic); Co= 0.042 (supersonic), CLmax = 1.7. a. Determine the corresponding velocity to the maximum producible load factor. b. Determine the maximum producible load factor. c. Determine the maximum producible bank angle.