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• W2058020153 abstract "An experimental investigation of first-ply failure and strength was conducted on ply-level scaled carbon/epoxy composite laminates having a stacking sequence of [+ϑn/−ϑ/−ϑn/90/902n]s where the constraint ply angle, ϑ, was varied from 0 to 75°, and where the constraint ply angle, ϑ, was varied from 0 to 75°, and n varied from 1 to 4. First-ply failure was shown to depend on the level of constraint and the scale factor, n. The strain energy release rate for matrix microcracking was computed from first-ply failure data of the [02/902]s laminate. Then, first-ply failure for all other layups was predicted using a numerical model that accounted for both constraint and size. Tensile strength was predicted using a strain energy release rate model for delamination of surface angle plies. A delamination energy value for each ply angle was calculated from the thinnest (n = 1) laminates to predict strength of the other sizes." @default.
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• W2058020153 date "2000-01-01" @default.
• W2058020153 modified "2023-09-25" @default.
• W2058020153 title "Scaling of First-Ply Failure and Strength in [+ϑn/−ϑ/−ϑn/90/902n]s Laminates: Experiments and Predictions" @default.
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• W2058020153 doi "https://doi.org/10.1520/ctr10635j" @default.
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