{"title":"静水压力下夹紧短椭圆形圆柱壳","authors":"W. P. Vafakos, F. Romano, J. Kempner","doi":"10.2514/8.9810","DOIUrl":null,"url":null,"abstract":"The principle of the minimum of the total potential is employed to obtain stresses and displacements for clamped, short, •oval cylindrical shells under hydrostatic pressure. Classical •shell theory, in which buckling effects are not considered, was used. A Fourier series is assumed for the deflections in the closed circumferential direction so tha t the partial differential equations of equilibrium are replaced by a set of ordinary differential equations. The energy solution is compared with a simplified approximation which can be considered an equivalent circular cylinder solution. Graphs of the significant stresses and displacements are presented for oval cylinders having major to minor axis ratios of 1.10, 1.30, and 1.50. It is shown tha t the maximum stresses and displacements increase significantly as the major to minor axis ratio is increased.","PeriodicalId":336301,"journal":{"name":"Journal of the Aerospace Sciences","volume":"16 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1962-11-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"16","resultStr":"{\"title\":\"Clamped Short Oval Cylindrical Shells Under Hydrostatic Pressure\",\"authors\":\"W. P. Vafakos, F. Romano, J. Kempner\",\"doi\":\"10.2514/8.9810\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The principle of the minimum of the total potential is employed to obtain stresses and displacements for clamped, short, •oval cylindrical shells under hydrostatic pressure. Classical •shell theory, in which buckling effects are not considered, was used. A Fourier series is assumed for the deflections in the closed circumferential direction so tha t the partial differential equations of equilibrium are replaced by a set of ordinary differential equations. The energy solution is compared with a simplified approximation which can be considered an equivalent circular cylinder solution. Graphs of the significant stresses and displacements are presented for oval cylinders having major to minor axis ratios of 1.10, 1.30, and 1.50. It is shown tha t the maximum stresses and displacements increase significantly as the major to minor axis ratio is increased.\",\"PeriodicalId\":336301,\"journal\":{\"name\":\"Journal of the Aerospace Sciences\",\"volume\":\"16 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1962-11-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"16\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Journal of the Aerospace Sciences\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.2514/8.9810\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Journal of the Aerospace Sciences","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.2514/8.9810","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Clamped Short Oval Cylindrical Shells Under Hydrostatic Pressure
The principle of the minimum of the total potential is employed to obtain stresses and displacements for clamped, short, •oval cylindrical shells under hydrostatic pressure. Classical •shell theory, in which buckling effects are not considered, was used. A Fourier series is assumed for the deflections in the closed circumferential direction so tha t the partial differential equations of equilibrium are replaced by a set of ordinary differential equations. The energy solution is compared with a simplified approximation which can be considered an equivalent circular cylinder solution. Graphs of the significant stresses and displacements are presented for oval cylinders having major to minor axis ratios of 1.10, 1.30, and 1.50. It is shown tha t the maximum stresses and displacements increase significantly as the major to minor axis ratio is increased.