{"title":"Design of domes for polymeric composite pressure vessels","authors":"M. Hojjati, V. Safavi Ardebili, S.V. Hoa","doi":"10.1016/0961-9526(95)93979-6","DOIUrl":null,"url":null,"abstract":"<div><p>The role of mechanical properties of composite material in dome contour design has been investigated. It has been shown that the optimal dome profile depends on the ratio of longitudinal Young's modulus to transverse Young's modulus in individual laminae (<em>E</em><sub><em>x</em></sub>/<em>E</em><sub><em>y</em></sub>). This profile for any type of composite material always lies between the Netting Analysis solution (<em>E</em><sub><em>y</em></sub> = 0, <em>E</em><sub><em>x</em></sub>/<em>E</em><sub><em>y</em></sub> =∞) and a semi-circle which is the solution for the square symmetric (<em>E</em><sub><em>x</em></sub>/<em>E</em><sub><em>y</em></sub> = 1) and isotropic materials. The shells of revolution of double curvature, classical lamination theory (CLT) and the geodesic-isotensoid assumptions have been used.</p></div>","PeriodicalId":100298,"journal":{"name":"Composites Engineering","volume":"5 1","pages":"Pages 51-59"},"PeriodicalIF":0.0000,"publicationDate":"1995-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://sci-hub-pdf.com/10.1016/0961-9526(95)93979-6","citationCount":"40","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Composites Engineering","FirstCategoryId":"1085","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/0961952695939796","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 40
Abstract
The role of mechanical properties of composite material in dome contour design has been investigated. It has been shown that the optimal dome profile depends on the ratio of longitudinal Young's modulus to transverse Young's modulus in individual laminae (Ex/Ey). This profile for any type of composite material always lies between the Netting Analysis solution (Ey = 0, Ex/Ey =∞) and a semi-circle which is the solution for the square symmetric (Ex/Ey = 1) and isotropic materials. The shells of revolution of double curvature, classical lamination theory (CLT) and the geodesic-isotensoid assumptions have been used.