A parametric study on supersonic/hypersonic flutter behavior of aero-thermo-elastic geometrically imperfect curved skin panel
In this paper, the effect of the system parameters on the flutter of a curved skin panel forced by a supersonic/hypersonic unsteady flow is numerically investigated. The aeroelastic model investigated includes the third-order piston theory aerodynamics for modeling the flow-induced forces and the Vo...
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Veröffentlicht in: | Acta mechanica 2011-11, Vol.222 (1-2), p.41-57 |
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Hauptverfasser: | , , , , |
Format: | Artikel |
Sprache: | eng |
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