氧化物/氧化物复合材料疲劳寿命建模

Procedia Engineering Pub Date : 2018-01-01 DOI:10.1016/j.proeng.2018.02.075

Orianne Sally , Cédric Julien , Frédéric Laurin , Rodrigue Desmorat , Florent Bouillon

{"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":null,"pages":null},"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\":null,\"pages\":null},\"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}

引用次数: 3

摘要

复合材料热结构件的使用寿命评估是航空工业的一个主要问题。为此，建立了编织复合材料在静、疲劳载荷作用下的统一损伤模型。它的特殊性在于它的速率损伤演化规律，它能够预测材料在循环或随机疲劳载荷下的行为。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

查看原文本刊更多论文

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.

求助全文

通过发布文献求助，成功后即可免费获取论文全文。去求助

来源期刊

Procedia Engineering

自引率

0.00%

发文量