A parametric study on supersonic/hypersonic flutter behavior of aero-thermo-elastic geometrically imperfect curved skin panel
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Publication:645329
DOI10.1007/s00707-011-0525-8zbMath1266.74025OpenAlexW2141493430MaRDI QIDQ645329
Laith K. Abbas, Roeland de Breuker, Xiao-Ting Rui, Piergiovanni Marzocca, Mostafa M. Abdalla
Publication date: 14 November 2011
Published in: Acta Mechanica (Search for Journal in Brave)
Full work available at URL: http://resolver.tudelft.nl/uuid:2de031f6-140b-49cb-aa83-27653c0c81c7
Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Thermal effects in solid mechanics (74F05) Stability of dynamical problems in solid mechanics (74H55) Supersonic flows (76J20) Hypersonic flows (76K05)
Related Items
Methods of continuation and their implementation in the COCO software platform with application to delay differential equations, Numerical investigation of aerothermoelastic characteristics of a thin heated panel in high supersonic and hypersonic flow, A parametric study on supersonic/hypersonic flutter behavior of aero-thermo-elastic geometrically imperfect curved skin panel, Aerothermoelastic analysis of panel flutter based on the absolute nodal coordinate formulation
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Cites Work
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