Question: The thrust required during the take-off is a function of __
Options
A : time
B : fuel
C : weight
D : lift
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Climb Rate more questions
Brequet Range expression value is maximum at __
Cruise climb technique is involved in ___
Drag raise is avoided by maintaining constant mach number.
In cruise method 1 the air pressure is decreased whereas....
The flight mach number is inversely proportional to relative pressure.
WAT anticipated changes result in better climb performance.
What is Brequet Range expression?
What is range factor in cruise method 1?
What is the condition of cruise method 1?
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