Aerospace Engineering > GATE 2016 > Aircraft Kinematics
The aircraft velocity (m/s) components in body axes are given as [u,v,w]=[100,10,10]. The air velocity (m/s), angle of attack (deg) and sideslip angle (deg) in that order are
A
[120, 0.1, 0.1]
B
[100, 0.1, 0.1]
C
[100.995, 0.1, 5.73]
D
[100.995, 5.71, 5.68]

Correct : d

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Related Topics

aircraft velocity components angle of attack sideslip angle Aerospace Engineering GATE 2016 GATE AE 2016 Q51 flight mechanics air velocity calculation aircraft dynamics

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