Aerospace Engineering > GATE 2009 > Stability and Control
An airplane flying at 100 m/s is pitching at the rate of 0.2 deg/s. Due to this pitching, the horizontal tail
surface located 4 metres behind the centre-of-mass of the airplane will experience a change in angle of
attack, which is
A
0.01 deg
B
0.008 deg
C
0.04 deg
D
0.004 deg

Correct : d

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