Stress analysis of a mode I edge delamination specimen for compositematerials

DOI10.2514/3.9408zbMath0594.73073OpenAlexW2073921824MaRDI QIDQ3725653

James M. Whitney

Publication date: 1986

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

Full work available at URL: https://doi.org/10.2514/3.9408

zbMATH Keywords

tensionstrain energy release ratetransverse shear deformationcompression loadingthermal residual stressesapproximate distribution of the interlaminar normal stresseffect of specimen geometryhigher-order laminated plate theorymode I edge delamination specimenthickness-stretch mode

Mathematics Subject Classification ID

Plates (74K20) Stress concentrations, singularities in solid mechanics (74G70) Composite and mixture properties (74E30) Thermal effects in solid mechanics (74F05) Brittle damage (74R05)

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