Optimum design of composite honeycomb sandwich panels subjected to uniaxial compression

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DOI10.2514/3.9502zbMath0598.73089OpenAlexW1966431601WikidataQ113256620 ScholiaQ113256620MaRDI QIDQ3733969

Jack R. Vinson

Publication date: 1986

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.9502

zbMATH Keywords

sandwich minimum weight face wrinkling cell size panels overall buckling core shear instability monocell buckling cell wall thickness Closed-form analytical solutions core depth hex-cell in-plane uniaxial compressive loads optimum face thickness overstressing square cell honeycomb core

Mathematics Subject Classification ID

Anisotropy in solid mechanics (74E10) Composite and mixture properties (74E30) Bifurcation and buckling (74G60) Optimization problems in solid mechanics (74P99)

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