Finite element analysis of Supersonic panel flutter
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Publication:5681610
DOI10.1002/nme.1620070313zbMath0265.73041OpenAlexW1997459654MaRDI QIDQ5681610
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Publication date: 1973
Published in: International Journal for Numerical Methods in Engineering (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1002/nme.1620070313
Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Plates (74K20) Finite element methods applied to problems in solid mechanics (74S05)
Related Items (9)
Numerical solution of large nonsymmetric eigenvalue problems ⋮ The Fluttering Panel as a Continuous Nonlinear Nonconservative System ⋮ Analysis of limit cycle oscillations of a typical airfoil section with freeplay ⋮ FLUTTER SUPPRESSION OF AN ELASTICALLY SUPPORTED PLATE WITH ELECTRO-RHEOLOGICAL FLUID CORE UNDER YAWED SUPERSONIC FLOWS ⋮ Effect of a bonded patch on aeroelastic behavior of cantilevered plates ⋮ Panel flutter analysis of plate element based on the absolute nodal coordinate formulation ⋮ Flutter instability of laminated thick anisotropic plates using BEM ⋮ CHAOTIC AND BIFURCATION DYNAMIC BEHAVIOR OF FUNCTIONALLY GRADED CURVED PANELS UNDER AERO-THERMAL LOADS ⋮ Flutter stabilization of cantilevered plates using a bonded patch
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