34th Congress of the International Council of the Aeronautical Sciences

03.3 - Basic Fluid Dynamics and Flow Control

A BRIEF REVIEW OF PANEL AEROELASTICITY WITH SHOCK INTERACTION

A. Shi, China; Y. He, China; E.H. Dowell, United States

Shock wave is inevitably encountered on flexible panel of high-speed vehicle. Severe pressure and thermal loads aggravate aeroelastic effect threatening structural safety. In turn, aeroelastic behaviors influence dynamics of shock. Via reviewing recent studies on panel aeroelasticity with shock from fluid-structure interaction and shock-boundary layer interaction, control strategies are motivated.


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