Affiliation:
1. Institute for Lightweight Engineering and Structural Mechanics (LSM), Department of Mechanical Engineering, Technical University Darmstadt, Darmstadt, Germany
Abstract
In this paper, the free-edge effects which play an important role in the failure analysis of composite laminates are studied. Pure temperature change and its combination with biaxial tension are investigated for a composite plate with a centric circular hole that is adequately small in comparison to the dimension of the plate. Moreover, the laminate is assumed to be thin, the temperature change of all points of the plate is identical and the biaxial tensile load is applied far from the center of the hole. For this purpose, a semi-analytical method based on a two-dimensional thermoelastic boundary layer theory and a minimum potential energy principle is proposed. It is shown that the present method predicts the interlaminar peeling and shear stresses surrounding the hole with good agreement compared to the results obtained by FEM analysis.
Subject
Materials Chemistry,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites