An unmanned radar-radio controlled aircraft with tilt-rotor propulsion is being designed
Chapter 7, Problem 7/34(choose chapter or problem)
An unmanned radar-radio controlled aircraft with tilt-rotor propulsion is being designed for reconnaissance purposes. Vertical rise begins with 0 and is followed by horizontal flight as approaches 90. If the rotors turn at a constant speed N of 360 rev/min, determine the angular acceleration of rotor A for 30 if is constant at 0.2 rad/s. 7/34
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