| contributor author | H. Murakami | |
| date accessioned | 2017-05-08T23:21:47Z | |
| date available | 2017-05-08T23:21:47Z | |
| date copyright | September, 1986 | |
| date issued | 1986 | |
| identifier issn | 0021-8936 | |
| identifier other | JAMCAV-26271#661_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/100744 | |
| description abstract | In order to improve the accuracy of the in-plane response of the shear, deformable laminated composite plate theory, a new laminated plate theory has been developed based upon a new variational principle proposed by Reissner (1984). The improvement is achieved by including a zigzag-shaped C 0 function to approximate the thickness variation of in-plane displacements. The accuracy of this theory is examined by applying it to a problem of cylindrical bending of laminated plates which has been solved exactly by Pagano (1969). The comparison of the in-plane response with the exact solutions for symmetric three-ply and five-ply layers has demonstrated that the new theory predicts the in-plane response very accurately even for small span-to-depth ratios. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Laminated Composite Plate Theory With Improved In-Plane Responses | |
| type | Journal Paper | |
| journal volume | 53 | |
| journal issue | 3 | |
| journal title | Journal of Applied Mechanics | |
| identifier doi | 10.1115/1.3171828 | |
| journal fristpage | 661 | |
| journal lastpage | 666 | |
| identifier eissn | 1528-9036 | |
| keywords | Composite materials | |
| keywords | Shear (Mechanics) | |
| keywords | Variational principles | |
| keywords | Plates (structures) AND Thickness | |
| tree | Journal of Applied Mechanics:;1986:;volume( 053 ):;issue: 003 | |
| contenttype | Fulltext | |
