\(\mathrm{C}^0\)-type global-local theory with non-zero normal strain for the analysis of thick multilayer composite plates

DOI10.1007/s00466-010-0554-5zbMath1398.74211OpenAlexW1988051098MaRDI QIDQ539436

Yong-Cai Geng, Sumit K. Garg

Publication date: 30 May 2011

Published in: Computational Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s00466-010-0554-5

zbMATH Keywords

thermal stresstransverse normal strain\(\mathrm{C}^0\)-type global-local theorymultilayer composite plate

Mathematics Subject Classification ID

Plates (74K20) Finite element methods applied to problems in solid mechanics (74S05) Composite and mixture properties (74E30) Thermal effects in solid mechanics (74F05) Bifurcation and buckling (74G60)

Cites Work

• Unnamed Item
• A finite element based on cubic zig-zag plate theory for the prediction of thermo-electric-mechanical behaviors
• A new discrete Kirchhoff quadrilateral element based on the third-order theory for composite plates
• Buckling analysis of angle-ply composite and sandwich plates by combination of geometric stiffness matrix
• Stability of sandwich plates by mixed, higher-order analytical formulation.
• Evaluation of transverse thermal stresses in composite plates based on first-order shear deformation theory
• A global-local higher order theory including interlaminar stress continuity and \(\text C^{0}\) plate bending element for cross-ply laminated composite plates
• A coupled zigzag theory for the dynamics of piezoelectric hybrid cross-ply plates
• A Simple Higher-Order Theory for Laminated Composite Plates
• Laminated Composite Plate Theory With Improved In-Plane Responses
• A higher order theory for extensional motion of laminated composites

This page was built for publication: \(\mathrm{C}^0\)-type global-local theory with non-zero normal strain for the analysis of thick multilayer composite plates