Effect of reinforced cutouts and ply-orientations on buckling behavior of composite panels subjected to non-uniform edge loads

DOI10.1142/S021945541850058XMaRDI QIDQ6493022

Y. M. Desai, T. Rajanna, Sauvik Banerjee, D. L. Prabhakara

Publication date: 26 April 2024

Published in: International Journal of Structural Stability and Dynamics (Search for Journal in Brave)

zbMATH Keywords

finite element methodbucklingcomposite laminateheterosis elementnon-uniform edge loadreinforced cutout

Mathematics Subject Classification ID

Bifurcation and buckling (74G60)

Related Items (1)

Determination of optimum effective parameters on thermal buckling of hybrid composite plates with quasi-square cut-out using a genetic algorithm

Cites Work

• Buckling analysis of laminated composite plates with an elliptical/circular cutout using FEM
• BUCKLING BEHAVIOR OF COMPOSITE LAMINATES (WITH AND WITHOUT CUTOUTS) SUBJECTED TO NONUNIFORM IN-PLANE LOADS
• On the Buckling of Isotropic, Transversely Isotropic and Laminated Composite Rectangular Plates
• Buckling Analysis of Mindlin Plates Under the Green–Lagrange Strain Hypothesis
• Stability and vibration of isotropic, orthotropic and laminated plates according to a higher-order shear deformation theory

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