Abstract
The low-velocity impact (LVI) test on the surface of the structural component may not be barely visible. However, it can cause severe structural damage and challenge the material’s damage resistance. The study of damage evolution and damage mechanism of the Kevlar fiber-reinforced polymer (KFRP) subjected to a three-point bending test after repeated LVI is the primary focus of this research. The KFRP laminates were subjected to single, triple, and penta-impact loadings with the same impact energy, and the specimens were subjected to a flexural test after impact. The results revealed that the through-thickness damage intensity increases with the number of impacts, reducing the material’s bending strength. The prominent damage mechanism was observed to be delamination induced through the impact, monitored through the acoustic emission (AE) sensors. The reduction of AE events noted during the delamination damage is 48.23, 55.49, and 96.36% in single, triple, and penta-impacted specimens compared with the nonimpacted specimens. The critical information provided here will help develop novel material capable of resisting repeated LVI, thus enhancing its mechanical strength.
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