5. For turbojet aircraft, the rate of climb is defined as: TayV – TregV RC mg Assume that you have a twin-jet aircraft with the following data: thrust of engine Tengine=31500N, velocity V=840km/h, mass m=72t, L/D=16, g=9.81m/s. Compute the thrust required to fly and then the rate of climb in m/s and ft/min. Is this condition suitable for the cruise point? Conversion: 1 m/s = 196.85 ft/min 1 m/s = 3.6 km/h
5. For turbojet aircraft, the rate of climb is defined as: TayV – TregV RC mg Assume that you have a twin-jet aircraft with the following data: thrust of engine Tengine=31500N, velocity V=840km/h, mass m=72t, L/D=16, g=9.81m/s. Compute the thrust required to fly and then the rate of climb in m/s and ft/min. Is this condition suitable for the cruise point? Conversion: 1 m/s = 196.85 ft/min 1 m/s = 3.6 km/h
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Transcribed Image Text:5. For turbojet aircraft, the rate of climb is defined as:
TayV – TregV
RC
mg
Assume that you have a twin-jet aircraft with the following data: thrust
of engine Tengine=31500N, velocity V=840km/h, mass m=72t, L/D=16,
g=9.81m/s. Compute the thrust required to fly and then the rate of climb
in m/s and ft/min. Is this condition suitable for the cruise point?
Conversion: 1 m/s = 196.85 ft/min
1 m/s = 3.6 km/h
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