| contributor author | K. Chandrashekhara | |
| contributor author | B. S. Kumar | |
| date accessioned | 2017-05-08T23:42:23Z | |
| date available | 2017-05-08T23:42:23Z | |
| date copyright | May, 1993 | |
| date issued | 1993 | |
| identifier issn | 0094-9930 | |
| identifier other | JPVTAS-28345#193_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/112544 | |
| description abstract | An approximate solution for a thick laminated simply supported circular cylindrical shell of revolution and shell panel subjected to asymmetric load has been obtained using elasticity approach. The results obtained from this analysis have been compared with the exact solution. Numerical results have been presented for 3-ply hybrid laminates and (0/90/0) laminates subjected to patch loads. The results have also been compared with some available classical and shear deformation theories to assess the accuracy of these theories. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Static Analysis of Thick Laminated Circular Cylindrical Shells | |
| type | Journal Paper | |
| journal volume | 115 | |
| journal issue | 2 | |
| journal title | Journal of Pressure Vessel Technology | |
| identifier doi | 10.1115/1.2929515 | |
| journal fristpage | 193 | |
| journal lastpage | 200 | |
| identifier eissn | 1528-8978 | |
| keywords | Circular cylindrical shells | |
| keywords | Laminates | |
| keywords | Stress | |
| keywords | Shear deformation | |
| keywords | Shells AND Elasticity | |
| tree | Journal of Pressure Vessel Technology:;1993:;volume( 115 ):;issue: 002 | |
| contenttype | Fulltext | |
