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- W3174802439 abstract "Fatigue damage in (0, + or - 45) and (0, + or - 45,90) boron/epoxy laminates was studied with X-ray radiography and scanning electron microscopy. In addition, limited tests for residual strength and stiffness were performed. The results of this study suggest that in boron/epoxy laminates the 45-degree plies play a key role in the fatigue process of boron/epoxy laminates that contain them. The fatigue process in the + or - 45-degree plies starts as intralaminar matrix cracks." @default.
- W3174802439 created "2021-07-05" @default.
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- W3174802439 date "1976-12-20" @default.
- W3174802439 modified "2023-09-26" @default.
- W3174802439 title "Fatigue damage of notched boron/epoxy laminates under constant amplitude loading" @default.
- W3174802439 hasPublicationYear "1976" @default.
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