Axisymmetric buckling and growth of a circular delamination in a compressed laminate

DOI10.1016/0020-7683(85)90011-3zbMath0571.73045OpenAlexW2029542579MaRDI QIDQ1061537

Wan-Lee Yin

Publication date: 1985

Published in: International Journal of Solids and Structures (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0020-7683(85)90011-3

zbMATH Keywords

iterative procedureaxisymmetric bucklingM-integralstability characteristicschange of the energy-release ratecircular delaminationcircular thinfilmcompressively loaded laminatefamily of nondimensionalized postbuckling solutionsfourth- order Runge-Kutta integration formulamidplane delaminationuniform-expansion growthvon Kármán's nonlinear plate theory

Mathematics Subject Classification ID

Plates (74K20) Bifurcation and buckling (74G60)

Related Items (12)

Calculation of energy release rate in composite delaminated cylindrical shells under circumferential concentrated dynamic load ⋮ On pressing of a buckled film ⋮ A finite element analysis of configurational stability and finite growth of buckling driven delamination ⋮ On problems of fracture of materials in compression along two internal parallel cracks ⋮ Nonlinear plate theory applied to delamination in composites ⋮ Analysis of energy release rate for composite delaminated cylindrical shells subjected to axial compression ⋮ Delamination growth of laminated circular plates under in-plane loads and movable boundary conditions ⋮ Delamination growth for composite laminated cylindrical shells under external pressure ⋮ Postbuckling analysis of stiffened laminated composite panels, using a higher-order shear deformation theory ⋮ A planar problem of failure of structural materials in compression along two parallel cracks ⋮ Modelling of laminates using a layerwise element with enhanced strains ⋮ Fracture mechanics of material in compression along cracks (review). Highly elastic materials

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