9.33 Consider a twin-turbofan-engine supersonic aircraft with the following characteristics: m = 18,000 kg, S= 40...

 

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9.33 Consider a twin-turbofan-engine supersonic aircraft with the following characteristics: m = 18,000 kg, S= 40 m, b = 14 m, Tax = 2 90 kN. Assume the maximum allowable load factor is 8 and a, = 0; C = 4.3 1/rad; e = 0.8, Cp = 0.018 (subsonic), Cp = 0.028 (transonic); C = 0.037 (supersonic), CLmax = 1.7. Is this fighter able to turn with a bank angle of 65, and a 1200 m of turn radius at 15,000 ft? If so, determine the time that it takes to have a 180 turn (a half circle). 9.33 Consider a twin-turbofan-engine supersonic aircraft with the following characteristics: m = 18,000 kg, S= 40 m, b = 14 m, Tax = 2 90 kN. Assume the maximum allowable load factor is 8 and a, = 0; C = 4.3 1/rad; e = 0.8, Cp = 0.018 (subsonic), Cp = 0.028 (transonic); C = 0.037 (supersonic), CLmax = 1.7. Is this fighter able to turn with a bank angle of 65, and a 1200 m of turn radius at 15,000 ft? If so, determine the time that it takes to have a 180 turn (a half circle).