=+mass (a simplified representation of the bending stiffness of the wing). The system possesses a rigid body
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=+mass (a simplified representation of the bending stiffness of the wing). The system possesses a rigid body mode for which the damping is assumed to be zero. You are asked to:
– For a wing eigenfrequency √ k
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Related Book For 
Mechanical Vibrations Theory And Application To Structural Dynamics
ISBN: 9781118900208
3rd Edition
Authors: Michel Geradin, Daniel J. Rixen
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