| contributor author | Chih-Ping Wu | |
| contributor author | Chi-Chuan Liu | |
| date accessioned | 2017-05-08T21:15:49Z | |
| date available | 2017-05-08T21:15:49Z | |
| date copyright | January 1995 | |
| date issued | 1995 | |
| identifier other | %28asce%290893-1321%281995%298%3A1%2843%29.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/44802 | |
| description abstract | A mixed finite-element scheme based on a discrete layer, high-order deformation theory is proposed, in this paper, for the analysis of thick, doubly curved laminated shells. The three-dimensional (3D) elasticity solutions of cross-ply cylindrical/spherical shells with shear diaphragm supports, subjected to a sinusoidally distributed normal load, are used for assessing the present finite-element scheme. Both the results obtained by full or reduced integration techniques and the convergence of the element are presented. The bending analyses of a variety of thick shells are discussed in the numerical examples. The finite-element solutions are compared with 3D elasticity solutions, and to other finite-element solutions related to global higher-order shell theories. The results indicate a close agreement with 3D elasticity solutions. | |
| publisher | American Society of Civil Engineers | |
| title | Mixed Finite-Element Analysis of Thick Doubly Curved Laminated Shells | |
| type | Journal Paper | |
| journal volume | 8 | |
| journal issue | 1 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)0893-1321(1995)8:1(43) | |
| tree | Journal of Aerospace Engineering:;1995:;Volume ( 008 ):;issue: 001 | |
| contenttype | Fulltext | |
