| contributor author | J. D. Stachiw | |
| contributor author | J. R. Maison | |
| date accessioned | 2017-05-08T22:59:27Z | |
| date available | 2017-05-08T22:59:27Z | |
| date copyright | February, 1975 | |
| date issued | 1975 | |
| identifier issn | 1087-1357 | |
| identifier other | JMSEFK-27618#1_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/87919 | |
| description abstract | The effects of an equatorial flange and a nonuniform wall thickness upon the critical pressure and stress distribution in acrylic plastic hemispheres have been investigated by experimental and analytical methods. Forty acrylic hemispheres were fabricated and tested to destruction under short term hydrostatic pressure applied on the convex surface. Dome apex displacements were obtained from each specimen and strains were obtained from a selected few. A finite element elastic analysis was performed on one window configuration for two different boundary conditions and the experimentally derived stresses were used to determine which boundary conditions was the best for analytical analysis. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Flanged Acrylic Plastic Hemispherical Shells for Undersea Application | |
| type | Journal Paper | |
| journal volume | 97 | |
| journal issue | 1 | |
| journal title | Journal of Manufacturing Science and Engineering | |
| identifier doi | 10.1115/1.3438537 | |
| journal fristpage | 1 | |
| journal lastpage | 9 | |
| identifier eissn | 1528-8935 | |
| keywords | Pressure | |
| keywords | Domes (Structural elements) | |
| keywords | Stress | |
| keywords | Hydrostatic pressure | |
| keywords | Stress concentration | |
| keywords | Flanges | |
| keywords | Analytical methods | |
| keywords | Finite element analysis | |
| keywords | Boundary-value problems | |
| keywords | Shells | |
| keywords | Wall thickness AND Elastic analysis | |
| tree | Journal of Manufacturing Science and Engineering:;1975:;volume( 097 ):;issue: 001 | |
| contenttype | Fulltext | |