{"title":"CFRP机身结构-允许后屈曲","authors":"Rolf Zimmermann , Raimund Rolfes","doi":"10.1016/S1290-0958(01)90075-9","DOIUrl":null,"url":null,"abstract":"<div><p>CFRP (carbon fibre reinforced plastics) fuselage structures are expected to be realized with future generations of aircraft. Going into the postbuckling regime with these structures requires improved, fast and reliable procedures for analysis and design of stiffened fibre composite panels. The EC project POSICOSS, which was started in the year 2000, develops such procedures. This article deals with the main objectives of the project, the theoretical and experimental work to be carried out, and with first results.</p></div>","PeriodicalId":100069,"journal":{"name":"Air & Space Europe","volume":"3 3","pages":"Pages 129-131"},"PeriodicalIF":0.0000,"publicationDate":"2001-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://sci-hub-pdf.com/10.1016/S1290-0958(01)90075-9","citationCount":"10","resultStr":"{\"title\":\"CFRP fuselage structures - postbuckling permitted\",\"authors\":\"Rolf Zimmermann , Raimund Rolfes\",\"doi\":\"10.1016/S1290-0958(01)90075-9\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><p>CFRP (carbon fibre reinforced plastics) fuselage structures are expected to be realized with future generations of aircraft. Going into the postbuckling regime with these structures requires improved, fast and reliable procedures for analysis and design of stiffened fibre composite panels. The EC project POSICOSS, which was started in the year 2000, develops such procedures. This article deals with the main objectives of the project, the theoretical and experimental work to be carried out, and with first results.</p></div>\",\"PeriodicalId\":100069,\"journal\":{\"name\":\"Air & Space Europe\",\"volume\":\"3 3\",\"pages\":\"Pages 129-131\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2001-05-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"https://sci-hub-pdf.com/10.1016/S1290-0958(01)90075-9\",\"citationCount\":\"10\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Air & Space Europe\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S1290095801900759\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Air & Space Europe","FirstCategoryId":"1085","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S1290095801900759","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
CFRP (carbon fibre reinforced plastics) fuselage structures are expected to be realized with future generations of aircraft. Going into the postbuckling regime with these structures requires improved, fast and reliable procedures for analysis and design of stiffened fibre composite panels. The EC project POSICOSS, which was started in the year 2000, develops such procedures. This article deals with the main objectives of the project, the theoretical and experimental work to be carried out, and with first results.
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