| contributor author | George A. Kardomateas | |
| date accessioned | 2017-05-08T21:16:02Z | |
| date available | 2017-05-08T21:16:02Z | |
| date copyright | July 2000 | |
| date issued | 2000 | |
| identifier other | %28asce%290893-1321%282000%2913%3A3%2885%29.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/44925 | |
| description abstract | An improved elasticity solution to the problem of buckling of orthotropic cylindrical shells subjected to external pressure is presented. The 2D axisymmetric cylindrical shell is studied (ring approximation). Specifically, in the development of the governing equations and boundary conditions for the buckling state, the solution includes the terms with the prebuckling normal strains and stresses as coefficients (i.e., the terms | |
| publisher | American Society of Civil Engineers | |
| title | Effect of Normal Strains in Buckling of Thick Orthotropic Shells | |
| type | Journal Paper | |
| journal volume | 13 | |
| journal issue | 3 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)0893-1321(2000)13:3(85) | |
| tree | Journal of Aerospace Engineering:;2000:;Volume ( 013 ):;issue: 003 | |
| contenttype | Fulltext | |
