Question 17 Ruforonewthe Frewmow the: In shown for s propeller circles In Figur 7.34. Find thursto of climb of 200 KTAS phunthe following Infemmetierc Which: - 20 003 lba. F1 2800 HP 2000 + 4000 Prop Airplane data Weight 20 000 lb Wing area (S) 500 f2 Sea level density o = 1 1500- 3000 325 Max endurance 3/2 FF min ~ HP, min ~ DV min . . Cp CL ) max 1000 Horsepower required = 2000 Horsepower required (HP.) Max endurance 500 + 1000 3/2 CL ) CD max Range max (FF) min = (HPI) min (DV) min . : ()max Fuel flow (Ib/hr) 0 100 200 300 Velocity (kts.)