| contributor author | Ahmed K. Noor | |
| contributor author | James H. Starnes, Jr. | |
| contributor author | Jeanne M. Peters | |
| date accessioned | 2017-05-08T22:17:11Z | |
| date available | 2017-05-08T22:17:11Z | |
| date copyright | October 2002 | |
| date issued | 2002 | |
| identifier other | 40096361.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/76252 | |
| description abstract | A study is made of the variability of the response of stiffened composite panels, associated with variations in the major geometric and material parameters of the structures. The major parameters, which have the most effect on the response quantities of interest, are identified by using a hierarchical sensitivity analysis. The range of variation of the response is determined by using a fuzzy set analysis, with the major parameters treated as fuzzy parameters. Numerical results are presented showing the variability of the response of panels with both continuous and terminated stiffeners associated with variations in the micromechanical, effective layer, and geometric parameters. Both flat and curved panels are considered. | |
| publisher | American Society of Civil Engineers | |
| title | Thermomechanical Response Variability of Stiffened Composite Panels | |
| type | Journal Paper | |
| journal volume | 15 | |
| journal issue | 4 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)0893-1321(2002)15:4(154) | |
| tree | Journal of Aerospace Engineering:;2002:;Volume ( 015 ):;issue: 004 | |
| contenttype | Fulltext | |
