Affiliation:
1. Department of Aeronautics and Astronautics Stanford University Stanford, California 94305
Abstract
An investigation was performed to study the mechanical response of fiber-reinforced thermoplastic matrix composites at elevated temperatures. The primary concern of the study was the effect of temperature on the viscoplastic behavior of the composites. During the investigation, an analytical model was developed for analyzing the response of both unidirectional and multidirectional composites at elevated temperatures. The model considers that the fibers have a linearly elastic behavior but the matrix responds viscoplastically with temperature. Micromechanics theories were adopted and developed to integrate fibers and matrix properties for predicting the response of unidirectional composites. Numerical algorithms were developed based on the lamination theory for evaluating the response of the laminated composites. Based on the model, a computer code was also developed for calculating the mechanical response of thermoplastic matrix composites subjected to both thermal and mechanical loading. In order to verify the model, experiments were also conducted for multidirectional APC-2 carbon/PEEK fiber composites and fairly good agreements were found between the predictions and the data.
Subject
Materials Chemistry,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites
Cited by
24 articles.
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