Aerospace Engineering > GATE 2014 > Aircraft Performance
Which of the following design parameters influence the maximum rate-of-climb for a jet-propelled airplane?
P. Wing loading
Q. Maximum thrust-to-weight ratio
R. Zero-lift drag coefficient
S. Maximum lift-to-drag ratio
A
P and Q alone
B
P, Q, R and S
C
P, Q and S alone
D
Q, R, and S alone

Correct : b

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Related Topics

maximum rate of climb jet propelled airplane GATE Aerospace Engineering 2014 aerospace engineering gate wing loading thrust weight ratio drag coefficient lift to drag ratio GATE 2014 airplane performance parameters

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