Parametric study on supersonic flutter of angle-ply laminated plates using shear deformable finite element method

DOI10.1007/S10409-011-0500-6zbMath1270.74101OpenAlexW1996230203MaRDI QIDQ362962

Mohammad Hasan, M. Dambrine

Publication date: 30 August 2013

Published in: Acta Mechanica Sinica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10409-011-0500-6

zbMATH Keywords

panel flutterfiber orientationangle-ply laminateslength-to-thickness ratioflow yaw angle

Mathematics Subject Classification ID

Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Plates (74K20) Finite element methods applied to problems in solid mechanics (74S05) Composite and mixture properties (74E30) Stability of dynamical problems in solid mechanics (74H55) Supersonic flows (76J20)

Cites Work

• A three-node Mindlin plate element with improved transverse shear
• Deteriorated geometrical stiffness for higher order finite elements with application to panel flutter
• A study on thermal postbuckling behaviour of laminated composite plates using a shear-flexible finite element
• Finite element analysis of large-amplitude panel flutter of thin laminates
• Nonlinear supersonic flutter of laminated composite plates under thermal loads

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