Flutter of Orthotropic Panels in Supersonic Flow Using Affine Transformations
DOI10.2514/3.60111zbMath0506.73054OpenAlexW2057058991MaRDI QIDQ4743849
Publication date: 1983
Published in: AIAA Journal (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.2514/3.60111
affine transformationsflutterlifting surface theorycomparedaerodynamic strip Ackeret theorybounded quantitiescertain defined characteristiccomprehensive solutionisotropic panels solution as subsetrectangular simply supported orthotropic panelssupersonic flow over one surface
Anisotropy in solid mechanics (74E10) Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Plates (74K20) Supersonic flows (76J20)
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