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Investigation of knitting architecture on the impact behavior of glass/epoxy composites
Affiliation:1. Istanbul University, Department of Mechanical Engineering, 34320 Istanbul, Turkey;2. Usak University, Department of Textile Engineering, 64200 Usak, Turkey;3. Usak University, Department of Mechanical Engineering, 64200 Usak, Turkey;1. College of Veterinary Medicine, Yangzhou University, Yangzhou, 225009, PR China;2. Jiangsu Co-innovation Center for Prevention and Control of Important Animal Infectious Diseases and Zoonoses, Yangzhou, 225009, PR China;3. Jiangsu Key Laboratory of Zoonosis, Yangzhou, 225009, PR China;4. Joint International Research Laboratory of Agriculture and Agri-Product Safety, The Ministry of Education of China, Yangzhou University, Yangzhou, 225009, PR China;5. The Department of Pediatric, The Affiliated Hospital of Yangzhou University, Yangzhou, 225009, PR China;1. Key Laboratory of High Performance Ship Technology (Wuhan University of Technology), Ministry of Education, Wuhan 430063, China;2. School of Transportation, Wuhan University of Technology, Wuhan 430063, China;1. The Ministry of Education Key Lab of Contemporary Design and Integrated Manufacturing Technology, Northwestern Polytechnical University, Xi’an 710072, China;2. Sustainable Manufacturing Systems Research Laboratory, Department of Mechanical and Industrial Engineering, University of Illinois at Chicago, Chicago 60607, USA;1. Old Dominion University, Norfolk, VA, USA;2. Johns-Manville Corp., Denver, CO, USA;3. The University of British Columbia, Vancouver, Canada
Abstract:In this study, the effect of impact and post-impact behavior of E-glass/epoxy composite plates having different knitted fabrics were investigated by considering energy profile diagram and the related load–deflection curves. Different impact energies (5–25 J) were subjected to the plates consisting of eight layers of Plain P]8, Milano M]8, and Rib R]8 knitted fabrics. The impact tests were continued until complete perforation of layer fabrics. The damage modes and damage processes of layer fabrics under varied impact energies were also discussed. At the end of the impact tests, the damaged samples were mounted into a compression apparatus to determine the Compression after Impact (CAI) strength of layer fabric samples. The results of these impact and post-impact tests showed that the maximum contact force was observed in the R]8 fabric and the minimum contact force was observed in the P]8 fabric and the CAI strength reduced by increasing the impact energy.
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