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This document is a dissertation submitted by Zhanming Qin to Virginia Polytechnic Institute and State University for the degree of Doctor of Philosophy in Engineering Mechanics. The dissertation investigates the vibration and aeroelasticity of advanced aircraft wings modeled as thin-walled beams, addressing dynamics, stability, and control. It develops analytical models for thin-walled beam structures and incorporates unsteady aerodynamic loads. State-space solutions are used to analyze dynamic aeroelastic

Author

sumanth_i

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EN