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- W2885598009 abstract "Abstract Drilling of composite material is a widely used operation in the aerospace industry. Despite of all precautions during the drilling process, the exit-ply delamination is still one of the major problems that affect the integrity and service life of the parts. The exit-ply delamination is directly related to the mechanical properties of composite materials as well as the nature of the induced thrust force along the cutting and chisel edges. In the current study, an attempt is made to model the induced thrust force. Both point and linear distributed loads models were utilized with consideration of elliptical delamination area. In order to validate the proposed model, a comparison between previous analytical models, measured forces, and the current proposed model is presented and discussed. The presented work was based on two scenarios. The first scenario considers the first mode of fracture only, while the second scenario considers the mixed- fracture mode criterion. The 1st scenario offers an average model accuracy about 77.9%, while the 2nd scenario offers an accuracy about 94.7% when compared to the predicted and measured data. It must be stated that both scenarios offer better prediction when compared to available model in the open literature. Thus, it can be concluded that the proposed model effectively demonstrates the delamination behaviour when drilling laminate composites." @default.
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- W2885598009 date "2018-01-01" @default.
- W2885598009 modified "2023-10-16" @default.
- W2885598009 title "Analytical Prediction of Delamination during Drilling Composite Laminates" @default.
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- W2885598009 doi "https://doi.org/10.1016/j.promfg.2018.07.032" @default.
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