Journal
COMPOSITES PART B-ENGINEERING
Volume 33, Issue 7, Pages 521-529Publisher
ELSEVIER SCI LTD
DOI: 10.1016/S1359-8368(02)00033-1
Keywords
laminates; strength; finite element analysis; joints; progressive damage modelling
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A parametric finite element analysis was conducted to investigate the effect of failure criteria and material property degradation rules on the tensile behaviour and strength of bolted joints in graphite/epoxy composite laminates. The analysis was based on a three-dimensional progressive damage model (PDM) developed earlier by the authors. The PDM comprises the components of stress analysis, failure analysis and material property degradation. The predicted load-displacement curves and failure loads of a single-lap single-bolt joint were compared with experimental data for different joint geometries and laminate stacking sequences. The stiffness of the joint was predicted with satisfactory accuracy for all configurations. The predicted failure load was significantly influenced by the combination of failure criteria and degradation rules used. A combination of failure criteria and material property degradation rules that leads to accurate strength prediction is proposed. For all the analyses performed, the macroscopic failure mechanism of the joint and the damage progression were also predicted. (C) 2002 Elsevier Science Ltd. All rights reserved.
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