The helicopter is nosing over at the constant rate q rad/s. If the rotor blades revolve
Chapter 7, Problem 7/30(choose chapter or problem)
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 of the rotor. Take the y-axis to be attached to the fuselage and pointing forward perpendicular to the rotor axis. 7/30
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