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Panel flutter is a self-excited oscillating phenomenon and involves interactions among elastic, inertia, and aerodynamic forces in supersonic flow. The panel flutter differs from wing flutter only in that the aerodynamic force resulting from the airflow acts only on one side of the panel. In the framework of small deflection linear structural theory, there is a critical speed of the airflow (or dynamic pressure λcr) beyond which the panel motion becomes unstable and grows exponentially with time.

Flutter Analysis of A Laminated Composite Plate with Temperature Dependent Material Properties