Multi-layer higher-order finite elements for the analysis of free-edge stresses in composite laminates

DOI<851::AID-NME312>3.0.CO;2-Q 10.1002/(SICI)1097-0207(19980315)41:5<851::AID-NME312>3.0.CO;2-QzbMath0903.73070OpenAlexW2072272758MaRDI QIDQ4398196

Paolo Gaudenzi, Rolando Carbonaro, A. Mannini

Publication date: 6 January 1999

Full work available at URL: https://doi.org/10.1002/(sici)1097-0207(19980315)41:5<851::aid-nme312>3.0.co;2-q

zbMATH Keywords

uniaxial tensionstacking sequences

Mathematics Subject Classification ID

Linear elasticity with initial stresses (74B10) Finite element methods applied to problems in solid mechanics (74S05) Composite and mixture properties (74E30)

Related Items (6)

Modal analysis of laminates by a mixed assumed-strain finite element model ⋮ MITC finite elements for laminated composite plates ⋮ Free-edge stress analysis of general composite laminates under extension, torsion and bending ⋮ A twofold strength and toughness criterion for the onset of free-edge shear delamination in angle-ply laminates ⋮ Three-dimensional stress analysis in torsion of laminated composite bar with general layer stacking ⋮ Thermal residual stresses in graded ceramic composites: a microscopic computational model versus homogenized models

Cites Work

• Edge singularities in anisotropic composites
• Stress fields in composite laminates
• On the Logarithmic Singularity of Free-Edge Stress in Laminated Composites Under Uniform Extension
• An Efficient Method for the Calculation of Interlaminar Stresses in Composite Materials
• Boundary-Layer Effects in Composite Laminates: Part 1—Free-Edge Stress Singularities
• Boundary-Layer Effects in Composite Laminates: Part 2—Free-Edge Stress Solutions and Basic Characteristics

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