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Failure simulation of integrated composite joint interface
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Aircraft Strength Research Insititute of Chaina
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Abstract:
Numerical finite element modelling techniques and failure analysis methods for integrated composite joint interface were studied. Different modelling techniques and failure models were adopt for joint interfaces bearing different loadings. The rule for defining interface mechanical properties was prescribed based on comparison between test results and simulations. The research of this paper can provide engineering utilizable analysis method for integrated composite structure design and analysis.
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ZHANG Aying. Failure simulation of integrated composite joint interface[J]. Advances in Aeronautical Science and Engineering,2013,4(4):509-514