{"title":"具有层间键合缺陷的层合平板的热力学响应","authors":"U. Icardi, M. Sciuva, L. Librescu","doi":"10.1115/imece1997-0723","DOIUrl":null,"url":null,"abstract":"\n In this study the problem of the implications played by the sliding interlaminar imperfections on the static and dynamic non-linear behavior of laminated composite flat panels subjected to thermomechanical loadings is addressed. Towards the end of approaching this problem, a recently developed geometrically non-linear theory of anisotropic composite flat panels featuring interlaminar bonding imperfections is used. A number of results related with the influence of interfacial bonding imperfections on the thermomechanical postbuckling and frequency-load-temperature interaction are supplied and pertinent conclusions are outlined.","PeriodicalId":403237,"journal":{"name":"Analysis and Design Issues for Modern Aerospace Vehicles","volume":"360 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1997-11-16","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"6","resultStr":"{\"title\":\"Thermomechanical Response of Laminated Flat Panels Featuring Interlaminar Bonding Imperfections\",\"authors\":\"U. Icardi, M. Sciuva, L. Librescu\",\"doi\":\"10.1115/imece1997-0723\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"\\n In this study the problem of the implications played by the sliding interlaminar imperfections on the static and dynamic non-linear behavior of laminated composite flat panels subjected to thermomechanical loadings is addressed. Towards the end of approaching this problem, a recently developed geometrically non-linear theory of anisotropic composite flat panels featuring interlaminar bonding imperfections is used. A number of results related with the influence of interfacial bonding imperfections on the thermomechanical postbuckling and frequency-load-temperature interaction are supplied and pertinent conclusions are outlined.\",\"PeriodicalId\":403237,\"journal\":{\"name\":\"Analysis and Design Issues for Modern Aerospace Vehicles\",\"volume\":\"360 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1997-11-16\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"6\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Analysis and Design Issues for Modern Aerospace Vehicles\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1115/imece1997-0723\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Analysis and Design Issues for Modern Aerospace Vehicles","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1115/imece1997-0723","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Thermomechanical Response of Laminated Flat Panels Featuring Interlaminar Bonding Imperfections
In this study the problem of the implications played by the sliding interlaminar imperfections on the static and dynamic non-linear behavior of laminated composite flat panels subjected to thermomechanical loadings is addressed. Towards the end of approaching this problem, a recently developed geometrically non-linear theory of anisotropic composite flat panels featuring interlaminar bonding imperfections is used. A number of results related with the influence of interfacial bonding imperfections on the thermomechanical postbuckling and frequency-load-temperature interaction are supplied and pertinent conclusions are outlined.
求助内容：
应助结果提醒方式：
京公网安备 11010802042870号
