A medium-sized jet has a 3.8-m-diameter fuselage and a loaded mass of 85,000 kg. The drag on an airplane is primarily due to the cylindrical fuselage, and aerodynamic shaping gives it a drag coefficient of 0.37. Part A How much thrust must the jetas engines provide to cruise at 290 m/s at an altitude where the air density is 1.9 kg/m³? Express your answer with the appropriate units. μA F = 157.35 KN

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A medium-sized jet has a 3.8-m-diameter fuselage and a loaded mass of 85,000 kg. The drag on an airplane is primarily
due to the cylindrical fuselage, and aerodynamic shaping gives it a drag coefficient of 0.37.
Part A
How much thrust must the jetas engines provide to cruise at 290 m/s at an altitude where the air density is
1.9 kg/m³?
Express your answer with the appropriate units.
0
μA
F = 157.35
KN
****
?
Transcribed Image Text:A medium-sized jet has a 3.8-m-diameter fuselage and a loaded mass of 85,000 kg. The drag on an airplane is primarily due to the cylindrical fuselage, and aerodynamic shaping gives it a drag coefficient of 0.37. Part A How much thrust must the jetas engines provide to cruise at 290 m/s at an altitude where the air density is 1.9 kg/m³? Express your answer with the appropriate units. 0 μA F = 157.35 KN **** ?
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