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- W3023641366 abstract "This chapter represents the author's contribution to Part B of the Failure Exercise. It explains graphs showing the theoretical predictions for failure envelopes and stress/strain diagrams of the 14 test cases. The successive failure of different laminates subjected to a variety of loading conditions is treated by a layer-by-layer failure analysis. Three sources of nonlinearity are considered—namely, material nonlinearity because of micro damage, matrix cracking, and changes in fiber angle with increasing strains. There is good agreement between predictions and experimental results. Some disagreement is because of imperfections in certain tests; therefore, these tests should be repeated. Three categories of laminate configuration/loading condition can be distinguished: (I) laminates with 3 or more fiber directions with arbitrary loading conditions; (II) balanced angle ply laminates with stress ratios in accordance with netting analysis; and (III) laminates with 2 fiber directions and loadings, which are not in accordance with netting analysis. The analysis of category (I) is straight forward. Category (II) is sensitive to the stiffness degradation after the onset of matrix cracking. Category (III) fails at low stresses and large strains of the laminate, because of a rapid deterioration. To define a failure limit for category (III), an intensive discussion is necessary. For the detection of the different modes (A, B, C) of inter-fiber fracture (IFF), refined action plane related IFF-criteria developed by Puck on the basis of Mohr's and Hashin's considerations on brittle fracture are explained." @default.
- W3023641366 created "2020-05-13" @default.
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- W3023641366 date "2004-01-01" @default.
- W3023641366 modified "2023-10-10" @default.
- W3023641366 title "Failure analysis of FRP laminates by means of physically based phenomenological models" @default.
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- W3023641366 doi "https://doi.org/10.1016/b978-008044475-8/50028-7" @default.
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