For the Gulfstream IV flying at an altitude of 39,360-ft, assuming weight of 73,000-lb. Airplane data: S = 950-ft2, AR = 5.92, CDo = 0.015, and K = 0.08. Calculate the minimum power required and the velocity at which it occurs. a. The PRmin. (in ft-lb/s) b. The velocity where PRmin occurs. (in ft/s)
For the Gulfstream IV flying at an altitude of 39,360-ft, assuming weight of 73,000-lb. Airplane data: S = 950-ft2, AR = 5.92, CDo = 0.015, and K = 0.08. Calculate the minimum power required and the velocity at which it occurs. a. The PRmin. (in ft-lb/s) b. The velocity where PRmin occurs. (in ft/s)
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For the Gulfstream IV flying at an altitude of 39,360-ft, assuming weight of 73,000-lb. Airplane data: S = 950-ft2, AR = 5.92, CDo = 0.015, and K = 0.08. Calculate the minimum power required and the velocity at which it occurs.
a. The PRmin. (in ft-lb/s)
b. The velocity where PRmin occurs. (in ft/s)
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