{"title":"氧化物/氧化物复合材料疲劳寿命建模","authors":"Orianne Sally , Cédric Julien , Frédéric Laurin , Rodrigue Desmorat , Florent Bouillon","doi":"10.1016/j.proeng.2018.02.075","DOIUrl":null,"url":null,"abstract":"<div><p>The assessment of service life of composite thermo-structural parts is a primary issue for the aeronautic industry. To this end, a unified damage model for woven composites undergoing both static and fatigue loadings is presented here. Its specificity resides in its rate damage evolution law, which enables to predict the behaviour of the material under cyclic or random fatigue loadings.</p></div>","PeriodicalId":20470,"journal":{"name":"Procedia Engineering","volume":"213 ","pages":"Pages 797-803"},"PeriodicalIF":0.0000,"publicationDate":"2018-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://sci-hub-pdf.com/10.1016/j.proeng.2018.02.075","citationCount":"3","resultStr":"{\"title\":\"Fatigue lifetime modeling of oxide/oxide composites\",\"authors\":\"Orianne Sally , Cédric Julien , Frédéric Laurin , Rodrigue Desmorat , Florent Bouillon\",\"doi\":\"10.1016/j.proeng.2018.02.075\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><p>The assessment of service life of composite thermo-structural parts is a primary issue for the aeronautic industry. To this end, a unified damage model for woven composites undergoing both static and fatigue loadings is presented here. Its specificity resides in its rate damage evolution law, which enables to predict the behaviour of the material under cyclic or random fatigue loadings.</p></div>\",\"PeriodicalId\":20470,\"journal\":{\"name\":\"Procedia Engineering\",\"volume\":\"213 \",\"pages\":\"Pages 797-803\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2018-01-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"https://sci-hub-pdf.com/10.1016/j.proeng.2018.02.075\",\"citationCount\":\"3\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Procedia Engineering\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S1877705818303102\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Procedia Engineering","FirstCategoryId":"1085","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S1877705818303102","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Fatigue lifetime modeling of oxide/oxide composites
The assessment of service life of composite thermo-structural parts is a primary issue for the aeronautic industry. To this end, a unified damage model for woven composites undergoing both static and fatigue loadings is presented here. Its specificity resides in its rate damage evolution law, which enables to predict the behaviour of the material under cyclic or random fatigue loadings.
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