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Three Failure Models for CFRP Composites
Technical Paper
2021-01-0310
ISSN: 0148-7191, e-ISSN: 2688-3627
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SAE WCX Digital Summit
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English
Abstract
Several failure criteria and stiffness degradation laws for composite materials are summarized and compared in terms of precision and convenience of use. The 2D/3D Hashin failure criteria are coupled with the stiffness degradation rules provided by Tan, Tserpes and Zinoviev. Three new failure models including 2D Hashin-Tan, 3D Hashin-Tser and 3D Hashin-Zin are presented for CFRP materials. The above three models were coded and incorporated into the ABAQUS software by user subroutines, among which model 2D Hashin-Tan and model 3D Hashin-Tser were programmed using the implicit algorithm VUSDFLD while model 3D Hashin-Zin was coded using the explicit algorithm VUMAT. Experiments of uniaxial tension and three-point bending were performed. A single element subjected to uniaxial tension and three-bending were simulated to check the function and precision of the new models. The simulation results show that the three models can predict the force-displacement response very well and the average precision of the new models was above 97% in the simulation of a plane plate subjected to uniaxial tension. Among the three models, the 2D Hashin-Tan model could predict the fibers/matrix failure due to tension/compression/shear except delamination. The 3D Hashin-Zinoviev model could well predict the delamination behavior of the CFRP plate. The 2D Hashin-Tan model and 3D Hashin-Tserpes model had the better computation efficiency than the 3D Hashin-Zinoviev model.
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Yu, H. and Wu, H., "Three Failure Models for CFRP Composites," SAE Technical Paper 2021-01-0310, 2021, https://doi.org/10.4271/2021-01-0310.Data Sets - Support Documents
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