Aerospace Engineering > GATE 2011 > Stability and Control
If an aircraft is performing a positive yawing manoeuvre, the side slip angle
A
is always zero
B
is never zero
C
is always negative
D
could be any value

Correct : b

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Related Topics

GATE AE 2011 Q16 GATE Aerospace Engineering 2011 positive yawing manoeuvre side slip angle aircraft flight mechanics aerospace flight dynamics yawing maneuver sideslip

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