| contributor author | Maher N. Bismarck-Nasr | |
| date accessioned | 2017-05-08T23:37:15Z | |
| date available | 2017-05-08T23:37:15Z | |
| date copyright | December, 1992 | |
| date issued | 1992 | |
| identifier issn | 0003-6900 | |
| identifier other | AMREAD-25636#461_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/109549 | |
| description abstract | A review of the finite element method applied to the problem of supersonic aeroelastic stability of plates and shells is presented. The review is limited to linear models. Some new contributions in the field are presented and future trends are discussed. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Finite Element Analysis of Aeroelasticity of Plates and Shells | |
| type | Journal Paper | |
| journal volume | 45 | |
| journal issue | 12 | |
| journal title | Applied Mechanics Reviews | |
| identifier doi | 10.1115/1.3119783 | |
| journal fristpage | 461 | |
| journal lastpage | 482 | |
| identifier eissn | 0003-6900 | |
| keywords | Aeroelasticity | |
| keywords | Finite element analysis | |
| keywords | Plates (structures) | |
| keywords | Shells | |
| keywords | Stability AND Finite element methods | |
| tree | Applied Mechanics Reviews:;1992:;volume( 045 ):;issue: 012 | |
| contenttype | Fulltext | |
