Question
Reference the P r curve that is shown for a propeller airplane in Figure 7.24. Find the angle of climb at 125 KTAS given the
Reference the Pr curve that is shown for a propeller airplane in Figure 7.24. Find the angle of climb at 125 KTAS given the following information: Weight=20000lbs. Pa=3500 HP
2000+ 1500 1000 500 = 4000 DV 325 Horsepower required: 3000 2000 1000 Prop Airplane data Weight 20 000 lb Wing area (S) 500 ft Sea level density o = 1 Max endurance FF min HP, min DV min r Max endurance 3/ 3/2 CL CD max Horsepower required (HP)
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Get StartedRecommended Textbook for
Organic Chemistry
Authors: David R. Klein
1st edition
047175739X , 9780471757399, 978-0470917800
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