Aerospace Engineering > GATE 2016 > Aircraft Performance
The load factor of an aircraft turning at a constant altitude is 2. The coefficient of lift required for turning flight as compared to level flight at the same speed will be
A
same
B
half
C
double
D
four times

Correct : c

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Related Topics

load factor aircraft aircraft turning flight coefficient of lift Aerospace Engineering GATE 2016 GATE AE 2016 Q25 lift coefficient turning flight aircraft performance turning aerodynamics load factor

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