desired to equip this airplane with turboprop engines with available power such that a maximi 602.6 mph at sea level can be reached. The available power is assumed to be independent of Calculate the maximum rate of climb and the speed at which it occurs. Given: W = 36,000 lb

Elements Of Electromagnetics
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1. An airplane weighs 36,000 lb. and has a wing area of 450 fte. The drag equation is C, =0.014 + 0.05C} . It is
desired to equip this airplane with turboprop engines with available power such that a maximum speed of
602.6 mph at sea level can be reached. The available power is assumed to be independent of flight speed.
Calculate the maximum rate of climb and the speed at which it occurs.
Given:
W = 36,000 lb
S = 450 ft²
C, = 0.014+0.05C
V = 602.6 mph
max
THPy = cons tan t
THP
AV
constant
Max EHP
Point of THP,
REQD.
Flisht Speed. V
Vmax 602.6 mph
Required:
Max R.C. and Vmax R.C.
Horsepower, hp
Transcribed Image Text:1. An airplane weighs 36,000 lb. and has a wing area of 450 fte. The drag equation is C, =0.014 + 0.05C} . It is desired to equip this airplane with turboprop engines with available power such that a maximum speed of 602.6 mph at sea level can be reached. The available power is assumed to be independent of flight speed. Calculate the maximum rate of climb and the speed at which it occurs. Given: W = 36,000 lb S = 450 ft² C, = 0.014+0.05C V = 602.6 mph max THPy = cons tan t THP AV constant Max EHP Point of THP, REQD. Flisht Speed. V Vmax 602.6 mph Required: Max R.C. and Vmax R.C. Horsepower, hp
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