Discuss the possibility of negative damping

Reference no: EM131783941

For a 1-DOF model of an airplane wing, assume an equation of the form

J₀θ"+cθ'+kθ=f₁(v,θ)+f₂(v,θ')

where θ is the angle of attack and v is the wind velocity.

Discuss the possibility of negative damping and the importance of the aerodynamic characteristics of the floor and stiffness girders for suspension bridges

The response must be typed, single spaced, must be in times new roman font (size 12) and must follow the APA format.

Reference no: EM131783941

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