Large-Amplitude Finite Element Flutter Analysis of Composite Panels in Hypersonic Flow

DOI10.2514/3.49051zbMath0779.73060OpenAlexW2149633413MaRDI QIDQ3134415

Chuh Mei, Carl E. Jun. Gray

Publication date: 7 September 1993

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://digitalcommons.odu.edu/mae_etds/232

zbMATH Keywords

third-order piston theorylimit-cycle amplitudevon Kármán large-deflection plate theory

Mathematics Subject Classification ID

Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Finite element methods applied to problems in solid mechanics (74S05) Composite and mixture properties (74E30) Hypersonic flows (76K05)

Related Items (3)

Nonlinear flutter of a two-dimension thin plate subjected to aerodynamic heating by differential quadrature method ⋮ A parametric study on supersonic/hypersonic flutter behavior of aero-thermo-elastic geometrically imperfect curved skin panel ⋮ Elastic plate in gas flow: Reducing from anisotropy to orthotropy

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