作者: Tomas Ireman , Tron Ranvik , Ingvar Eriksson
DOI: 10.1016/S0263-8223(99)00130-0
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摘要: Abstract A comprehensive experimental program was conducted to measure and characterize the development of damage in vicinity fastener holes graphite/epoxy composite laminates. This carried out generate data which can be used for appropriate failure criteria. Test specimens were loaded quasi-static cycles with successively increasing loads, bolt detected using different methods such as strain measurements, acoustic emission, X-ray microscopic examination. Several modes a series events starting at load levels far below level first visible evidence appeared on load–displacement curve. Failure included matrix cracking, fibre fracture, delamination kinking.