Buckling of Laminated Cylindrical Panels Under Uniaxial CompressionSource: Journal of Energy Resources Technology:;1991:;volume( 113 ):;issue: 004::page 250Author:K. Chandrashekhara
DOI: 10.1115/1.2905908Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Buckling characteristics of anisotropic laminated cylindrical panels are presented using an isoparametric nine-noded rectangular element. Kinematic relations, extended to include the first-order shear deformation theory, are utilized in the formulation. Numerical results are presented for laminated cylindrical panels under uniaxial compression loading to illustrate the influence of panel sizes, orientation of layers, material properties, and boundary conditions on the buckling loads. Results for plates are also presented as special cases and are compared with the available solutions.
keyword(s): Buckling , Compression , Shear deformation , Stress , Materials properties , Plates (structures) AND Boundary-value problems ,
|
Collections
Show full item record
| contributor author | K. Chandrashekhara | |
| date accessioned | 2017-05-08T23:35:20Z | |
| date available | 2017-05-08T23:35:20Z | |
| date copyright | December, 1991 | |
| date issued | 1991 | |
| identifier issn | 0195-0738 | |
| identifier other | JERTD2-26440#250_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/108430 | |
| description abstract | Buckling characteristics of anisotropic laminated cylindrical panels are presented using an isoparametric nine-noded rectangular element. Kinematic relations, extended to include the first-order shear deformation theory, are utilized in the formulation. Numerical results are presented for laminated cylindrical panels under uniaxial compression loading to illustrate the influence of panel sizes, orientation of layers, material properties, and boundary conditions on the buckling loads. Results for plates are also presented as special cases and are compared with the available solutions. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Buckling of Laminated Cylindrical Panels Under Uniaxial Compression | |
| type | Journal Paper | |
| journal volume | 113 | |
| journal issue | 4 | |
| journal title | Journal of Energy Resources Technology | |
| identifier doi | 10.1115/1.2905908 | |
| journal fristpage | 250 | |
| journal lastpage | 253 | |
| identifier eissn | 1528-8994 | |
| keywords | Buckling | |
| keywords | Compression | |
| keywords | Shear deformation | |
| keywords | Stress | |
| keywords | Materials properties | |
| keywords | Plates (structures) AND Boundary-value problems | |
| tree | Journal of Energy Resources Technology:;1991:;volume( 113 ):;issue: 004 | |
| contenttype | Fulltext |