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Nonlinear supersonic flutter of panels considering shear deformation and rotary inertia
Authors:K.Singa Rao  G.Venkatewsara Rao
Affiliation:Aerospace Structures Division, Vikram Sarabhai Space Centre, Trivandrum 695022, India
Abstract:Nonlinear supersonic flutter of panels is studied for end conditions of simply supported, clamped and partial restraint against rotation by a unified approach. The effect of shear deformation and rotary inertia on nonlinear flutter boundary is studied for various thicknesses of panel.
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