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- W3082908970 abstract "Automated Fiber Placement is one of the well-established composite fabrication techniques in both aerospace and automotive industries. However, new types of defects may be formed during the fiber steering due to replacing the prepreg sheets with the prepreg fiber tows. These defects can be a source of both intralaminar and interlaminar damages, which reduce the mechanical performance of the final products. Although the effect of these defects on the performance of the composite structure, especially the in-plane behavior can be found in the literature, there is still a lack of knowledge in the study of the mechanical performance of the composite structures with manufacturing induced defects . In the present study, the effect of automated manufacturing induced gaps on the mechanical response and failure of the Quasi-isotropic Carbon/Epoxy thin beams under out-of-plane loading is investigated. For this purpose, three-point bending tests are carried out on both short and standard beams to measure the interlaminar shear strength and flexural stiffness/strength of the composite beams with the gaps. The results are then compared with the results of the baseline sample (the one with no defect). Furthermore, Finite Element simulations are used to examine the stress distribution and also damage initiation and propagation of the composite beams under out-of-plane loading in the presence of the gaps. It is shown that the material scaling at the inhomogeneity area, which is widely used in the literature for Finite Element simulation of the composite structure with the gaps, is not sufficient for all scenarios of the loading and thickness scaling might also be applied to the models." @default.
- W3082908970 created "2020-09-08" @default.
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- W3082908970 date "2020-11-01" @default.
- W3082908970 modified "2023-09-24" @default.
- W3082908970 title "Flexural response of composite beams made by Automated Fiber Placement process: Effect of fiber tow gaps" @default.
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- W3082908970 doi "https://doi.org/10.1016/j.compositesb.2020.108368" @default.
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