Aerothermoelastic analysis of lattice sandwich composite panels in supersonic airflow

DOI10.1007/s11012-015-0240-yzbMath1338.74041OpenAlexW965429956MaRDI QIDQ296080

Feng-Ming Li, Zhi-Guang Song

Publication date: 14 June 2016

Published in: Meccanica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s11012-015-0240-y

zbMATH Keywords

aerothermoelasticlattice sandwich composite panelpyramidal truss coresupersonic airflowtriangular grid core

Mathematics Subject Classification ID

Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Composite and mixture properties (74E30) Supersonic flows (76J20)

Related Items

Computation of aerothermoelastic properties and active flutter control of CNT reinforced functionally graded composite panels in supersonic airflow, Nonlinear primary resonances of lattice sandwich beams with pyramidal truss core and viscoelastic surfaces

Cites Work

• Preliminary assessment of sandwich plates subject to blast loads.
• Heat transfer efficiency of metal honeycombs
• Aeroelastic analysis and active flutter control of nonlinear lattice sandwich beams
• Nonlinear panel flutter using high-order triangular finite elements
• Finite element nonlinear panel flutter with arbitrary temperatures in supersonic flow