Simple Bending Analysis of Laminated Plates by Large-Deflection Theory
- 1 March 1970
- journal article
- Published by SAGE Publications in Journal of Composite Materials
- Vol. 4 (3) , 380-389
- https://doi.org/10.1177/002199837000400309
Abstract
A closed-form solution is presented for the problem of laminated plates subjected to simple bending by the application of the nonlinear von Karman equations of heterogeneous anisotropic plates. The coupling effect between in-plane extension and transverse bending of cross-ply and angle-ply laminates on the cross-sectional distortion of the bent plates is studied. The results of the cases of two-layer com posite of orthotropic material are obtained, it shows that cross-ply of layers with high tensile moduli ratio can greatly reduce the peak-to- trough deflection of the cross section of a bent laminated plate.Keywords
This publication has 12 references indexed in Scilit:
- Exact Solutions for Rectangular Bidirectional Composites and Sandwich PlatesJournal of Composite Materials, 1970
- Analysis of a simply supported laminated anisotropic rectangular plateAIAA Journal, 1970
- Cylindrical Bending of Unsymmetrically Laminated PlatesJournal of Composite Materials, 1969
- Exact Solutions for Composite Laminates in Cylindrical BendingJournal of Composite Materials, 1969
- Optimization study of anticlastic curvature of cylindrically bent strips with variable thicknessInternational Journal of Mechanical Sciences, 1969
- Bending-Extensional Coupling in Laminated Plates Under Transverse LoadingJournal of Composite Materials, 1969
- A Generalized Analysis of Conically Bent Plates by Large-Deflection TheoryJournal of Applied Mechanics, 1968
- Bending and Stretching of Certain Types of Heterogeneous Aeolotropic Elastic PlatesJournal of Applied Mechanics, 1961
- ANALYSIS OF STRUCTURAL LAMINATESPublished by Defense Technical Information Center (DTIC) ,1961
- The Anticlastic Curvature of Rectangular Beams and PlatesJournal of the Royal Aeronautical Society, 1950