| タイトル | Multilayer theory for delamination analysis of a composite curved bar subjected to end forces and end moments |
| 本文（外部サイト） | http://hdl.handle.net/2060/19900003353 |
| 著者（英） | Jackson, Raymond H.; Ko, William L. |
| 著者所属（英） | NASA Dryden Flight Research Facility |
| 発行日 | 1989-09-01 |
| 言語 | eng |
| 内容記述 | A composite test specimen in the shape of a semicircular curved bar subjected to bending offers an excellent stress field for studying the open-mode delamination behavior of laminated composite materials. This is because the open-mode delamination nucleates at the midspan of the curved bar. The classical anisotropic elasticity theory was used to construct a multilayer theory for the calculations of the stress and deformation fields induced in the multilayered composite semicircular curved bar subjected to end forces and end moments. The radial location and intensity of the open-mode delamination stress were calculated and were compared with the results obtained from the anisotropic continuum theory and from the finite element method. The multilayer theory gave more accurate predictions of the location and the intensity of the open-mode delamination stress than those calculated from the anisotropic continuum theory. |
| NASA分類 | COMPOSITE MATERIALS |
| レポートNO | 90N12669
NASA-TM-4139
NAS 1.15:4139
H-1490 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/139831 |
