Eigenvalue problem for integro-differential equation of supersonic panel flutter

DOI10.1007/BF01875890zbMath0598.76071OpenAlexW2070546120WikidataQ115393125 ScholiaQ115393125MaRDI QIDQ1080315

Ming-de Dong

Publication date: 1984

Published in: Applied Mathematics and Mechanics. (English Edition) (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf01875890

zbMATH Keywords

complex eigenvalue problemcritical curveaeroelastic systemsupersonic flutterExact solutionsblade cascade in turbo-generatordegeneracy of critical Mach numberdynamic stability of a thin platelow supersonic regionmutual separation of flutternon-self-adjoint fourth-order integro-differential equation of Volterra's typethree-dimensional airfoil modeltwo-dimensional linear theoryvacuum frequency spectrums

Mathematics Subject Classification ID

Integro-ordinary differential equations (45J05) Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Supersonic flows (76J20) Eigenvalue problems for integral equations (45C05)

Cites Work

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• Coupled Bending-Torsion Flutter in a Supersonic Cascade

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