Affiliation:
1. School of Aeronautics and Astronautics Purdue University West Lafayette, IN 47907-1282, USA
Abstract
The nonlinear behavior of AS4/PEEK composite under off-axis loading was investigated using a finite element-based micromechanical approach with three different unit cells. Proper boundary conditions for uniaxial off-axis loading for the unit cell were established. The elastic moduli of the fiber and the nonlinear stress-strain curve of the matrix were used in the micromechanical analysis. By comparing the predicted off-axis stress-strain curves with experimental data, it was found that the nonlinear behavior of the composite is highly dependent on the fiber packing arrangement of the unit cell model.
Subject
Condensed Matter Physics,Ceramics and Composites
Cited by
9 articles.
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