Aerospace Engineering > GATE 2016 > Aircraft Stability
The Dutch roll motion of the aircraft is described by following relationship
The undamped natural frequency (rad/s) and damping ratio for the Dutch roll motion in that order are:
A
4.68, 1.02
B
4.49, 1.02
C
2.165, 0.235
D
2.165, 1.02

Correct : c

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Related Topics

Dutch roll motion aircraft dynamics undamped natural frequency damping ratio Aerospace Engineering GATE 2016 GATE AE 2016 Q52 aircraft stability and control second order system

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