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500 Fuel flow (lb/hr) 1000 2000 4000 1500 Horsepower 2000 1000 3000 Prop airplane data Wing area (S) 500 ft Sea level density =
500 Fuel flow (lb/hr) 1000 2000 4000 1500 Horsepower 2000 1000 3000 Prop airplane data Wing area (S) 500 ft Sea level density = 1 (L/D) max 100 (LD) max Velocity (kts.) 200 W=30000 lb W = 20000 lb 300
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Fundamentals of Heat and Mass Transfer
Authors: Incropera, Dewitt, Bergman, Lavine
6th Edition
978-0470055540, 471457280, 470881453, 470055545, 978-0470881453, 978-0471457282
