The helicopter is nosing over at the constant rate q rad/s. If the rotor blades revolve at
Question:
The helicopter is nosing over at the constant rate q rad/s. If the rotor blades revolve at the constant speed p rad/s, write the expression for the angular acceleration a of the rotor. Take the y-axis to be attached to the fuselage and pointing forward perpendicular to the rotor axis.
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The angular acceleration of the rotor is given by the following equation a pq Ex...View the full answer
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Related Book For 
Engineering Mechanics Dynamics
ISBN: 9781118885840
8th Edition
Authors: James L. Meriam, L. G. Kraige, J. N. Bolton
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