Drilling of composites is currently rife with damage phenomenon such as spalling, delamination, edge chipping, fiber pull-outs, crack formation, thermal residual stresses and excessive tool wear.

Exit-ply delamination has been identified as the most deleterious damage

phenomenon for structural components as it results in a significant loss of strength and stiffness of the laminate and, consequently its load carrying capacity. Identification and prevention of delamination therefore becomes particularly important for composite components subjected to compressive, shear.

it has been seen that the main cause of delamination is thrust force and feed rate, so by obtaining critical values of these parameters we can reduce delamination.

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