A theory for stress analysis of composite laminates

DOI10.2514/3.9045zbMath0575.73084OpenAlexW2080868426MaRDI QIDQ3694813

L. W. Rehfield, R. Rao Valisetty

Publication date: 1985

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

Full work available at URL: https://doi.org/10.2514/3.9045

zbMATH Keywords

transverse normal straindelaminationthree-dimensionalcross-ply laminatesection warpingbending theoryFailuresarbitrary composite laminatesconcomitant nonclassical surface- parallel stress contributionscontrolled by interlaminar stresseslaminated resin matrix composite materialsmatrix microcrackingmodes of damagequasi-isotropic laminatereliable stress estimates in critical regions

Mathematics Subject Classification ID

Plates (74K20) Stress concentrations, singularities in solid mechanics (74G70) Composite and mixture properties (74E30)

Related Items (1)

Postbuckling analysis of stiffened laminated composite panels, using a higher-order shear deformation theory

This page was built for publication: A theory for stress analysis of composite laminates