Plot the thrust required at sea level

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Question:

Using the Global Hawk aircraft, wing span of 116 ft, gross weight of 26,750, max takeoff weight is 32350 lbs, fuel capacity of 17,300 lbs, Power Plant is Rolls Royce-North American F137-RR-100 turbofan engine, thrust is 7600 lbs and drag coeffient of 0.02 + 0.062C(2/L).

Plot the thrust required at sea level and at 10000 ft and obtain obtain max velocity at sea level and 10000 ft. Discuss what these results tell us about your aircraft.

Reference no: EM132475634

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