Linear and non-linear failure analysis of composite laminates with transverse shear

• Published in: Composites science and technology 1992, Vol.44 (3), p.227-255
• Main Authors: Reddy, Y.S.N., Reddy, J.N.
• Format: Article
• Language: English
• Subjects: Applied sciences; composite laminate; composite materials; Exact sciences and technology; failure; finite element method; first-ply failure load; Forms of application and semi-finished materials; Laminates; loading; non-linear failure analysis; phenomenological failure criteria; Polymer industry, paints, wood; shear strength; Structural Mechanics; Technology of polymers; transverse shear
• ISSN: 0266-3538; 1879-1050
• DOI: 10.1016/0266-3538(92)90015-U

A finite element computational procedure has been developed to find linear and non-linear (von Kármán) first-ply failure loads of composite laminates subjected to in-plane and transverse loads. The finite element model is based on first-order shear deformation theory and several phenomenological failure criteria. Linear and non-linear first-ply failure loads are computed for a uniformly distributed transverse load, a concentrated transverse load acting at the centre of the plate, and a uniformly distributed in-plane edge load for simply supported and clamped boundary conditions. It is found that the failure loads predicted by various failure criteria differ from one another by a maximum of 35% in the case of linearloads and 50% in the case on non-linear loads; the failure locations differ from each other in a random way. Furthermore, it is demonstrated that the difference between the linear and non-linear failure loads is large in the case of transversely loaded simply supported laminates and thin plates. The difference is found to be quite small in the case of in-plane (tensile) loading and thick laminates.