Aerospace Engineering > GATE 2011 > Climb Performance
Lift on an aircraft climbing vertically up is
A
equal to its weight
B
zero
C
equal to the drag
D
equal to the thrust

Correct : b

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Related Topics

GATE Aerospace Engineering 2011 Q15 GATE Aerospace Engineering 2011 lift on an aircraft climbing vertically up aircraft vertical climb forces lift force in vertical flight aerodynamics aircraft performance forces on climbing aircraft

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