{"title":"碳纤维增强PEEK弯曲疲劳损伤发展","authors":"G. Dillon, M. Buggy","doi":"10.1016/S0010-4361(06)80135-7","DOIUrl":null,"url":null,"abstract":"<div><p>Fatigue damage growth mechanisms in [0]<sub>16</sub> and [0, 90]<sub>4s</sub> laminates of APC-2 subjected to three-point flexure were studied using scanning electron microscopy. Building on an understanding gained from the study of statically tested samples, specific fatigue mechanisms were identified. For each laminate geometry a coherent progression of damage build-up is proposed.</p></div>","PeriodicalId":100296,"journal":{"name":"Composites","volume":"26 5","pages":"Pages 355-370"},"PeriodicalIF":0.0000,"publicationDate":"1995-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://sci-hub-pdf.com/10.1016/S0010-4361(06)80135-7","citationCount":"21","resultStr":"{\"title\":\"Damage development during flexural fatigue of carbon fibre-reinforced PEEK\",\"authors\":\"G. Dillon, M. Buggy\",\"doi\":\"10.1016/S0010-4361(06)80135-7\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><p>Fatigue damage growth mechanisms in [0]<sub>16</sub> and [0, 90]<sub>4s</sub> laminates of APC-2 subjected to three-point flexure were studied using scanning electron microscopy. Building on an understanding gained from the study of statically tested samples, specific fatigue mechanisms were identified. For each laminate geometry a coherent progression of damage build-up is proposed.</p></div>\",\"PeriodicalId\":100296,\"journal\":{\"name\":\"Composites\",\"volume\":\"26 5\",\"pages\":\"Pages 355-370\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1995-05-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"https://sci-hub-pdf.com/10.1016/S0010-4361(06)80135-7\",\"citationCount\":\"21\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Composites\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S0010436106801357\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Composites","FirstCategoryId":"1085","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0010436106801357","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Damage development during flexural fatigue of carbon fibre-reinforced PEEK
Fatigue damage growth mechanisms in [0]16 and [0, 90]4s laminates of APC-2 subjected to three-point flexure were studied using scanning electron microscopy. Building on an understanding gained from the study of statically tested samples, specific fatigue mechanisms were identified. For each laminate geometry a coherent progression of damage build-up is proposed.
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