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
Correct : d
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An aircraft is flying with inertial ground and wind speeds of v→gb=(100,5,5)m/s and v→wb=(0,-5,-10)m/s, respectively, as expressed in the body frame....
An aircraft is flying with inertial ground and wind speeds of v→gb=(100,5,5)m/s and v→wb=(0,-5,-10)m/s, respectively, as expressed in the body frame....
An aircraft is flying with inertial ground and wind speeds of v→gb=(100,5,5)m/s and v→wb=(0,-5,-10)m/s, respectively, as expressed in the body frame....
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