The helicopter is nosing over at the constant rate q rad/s. If the rotor blades revolve at

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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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Engineering Mechanics Dynamics

ISBN: 9781118885840

8th Edition

Authors: James L. Meriam, L. G. Kraige, J. N. Bolton

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