Aerothermoelastic analysis of curvilinear fiber variable stiffness laminated panels in supersonic flow

DOI10.1007/s00707-022-03331-2zbMath1504.74015OpenAlexW4296311921MaRDI QIDQ2092914

Jingbo Duan, Buqing Xu, Yihang Gao, Yong-Jun Lei

Publication date: 4 November 2022

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

Full work available at URL: https://doi.org/10.1007/s00707-022-03331-2

zbMATH Keywords

finite element methodfluttervirtual work principlethermal bucklingNewmark methodfirst-order aerodynamic piston theoryMindlin thick plate theory

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) Thermal effects in solid mechanics (74F05) Stability of dynamical problems in solid mechanics (74H55) Supersonic flows (76J20)

Related Items (1)

Snap-through response of three-dimensional braided composite panels in thermal-acoustic-aero coupled field

Cites Work

• Aeroelastic flutter analysis for 2D Kirchhoff and Mindlin panels with different boundary conditions in supersonic airflow
• Multimode Approach to Nonlinear Supersonic Flutter of Imperfect Circular Cylindrical Shells
• Nonlinear Vibrations and Stability of Shells and Plates
• In-plane response of laminates with spatially varying fiber orientations - Variable stiffness concept
• Nonlinear Mechanics of Shells and Plates in Composite, Soft and Biological Materials
• Finite element time domain - Modal formulation for nonlinear flutter of composite panels

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