A propeller-driven plane, having the following
characteristics:
A Propeller Driven Plane Having The Following Characteristics Calculate The Maximum Rate Of Clime R C Max At Sea Leve 1 (254.44 KiB) Viewed 12 times
Calculate the maximum rate of
clime (R/C)max at sea-level standard
conditions and maximum weight. Assume the engine power and
propeller efficiency do not vary with velocity
W = 1100 kg Сp,0 = 0.045 S = 18 m2 n = 0.8 b = 12 m = 150 kW Pmax e = 0.75 SFC = 3 N/kW/hr Calculate the maximum rate of climb (R/C)mar at sea-level standard conditions and maximum weight. Assume the engine power and propeller efficiency do not vary with velocity.
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