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- W2356400076 abstract "The paper analyses finite element theory which compute final intensity of composite laminate,and discusses modified Newton-Raphson iterative method for stress field computation in the process of laminate failure.As the same time,the paper develops the three-dimensional finite element model with notch and considers three failure modes of laminate such as fiber breakage,matrix crack and delamination.The modified three-dimensional Hashin criterion is taken as criterion of judging failure,the paper calculates ultimate loading values of three different stacking laminate.An excellent agreement is found between the predictions and the experimental data.Due to the uncertainty of material property ν23,its influence on failure analysis is studied.At last,the failure propagation progression is simulated.studies finite element theory for calculating ultimate intensity of composite laminate,and discusses modified Newton-Raphson iterative method for stress field computation in the process of laminate failure.As the same time,the paper develops the three-dimensional(3D) finite element model with notch,and considers three failure modes of laminate such as fiber breakage,matrix crack and delamination.The modified 3D Hashin criterion is taken as criterion of judging failure,the paper calculates ultimate loading values of three different stacking laminate.An excellent agreement is found between the predictions and the experimental data.Due to the uncertainty of material property" @default.
- W2356400076 created "2016-06-24" @default.
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- W2356400076 date "2008-01-01" @default.
- W2356400076 modified "2023-09-24" @default.
- W2356400076 title "Three-dimensional Finite Element Failure Analysis of Notched Composite Laminates" @default.
- W2356400076 hasPublicationYear "2008" @default.
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