| タイトル | Effect of laminate thickness and specimen configuration on the fracture of laminated composites |
| 著者（英） | Harris, C. E.; Morris, D. H. |
| 著者所属（英） | Virginia Polytechnic Inst. and State Univ.|Texas A&M Univ. |
| 発行日 | 1986-01-01 |
| 言語 | eng |
| 内容記述 | Attention is given to the effect of laminate thickness on graphite/epoxy laminates in the present measurements of fracture toughness in center cracked tension specimens, compact tension specimens, and three-point bend specimens. Crack tip damage development prior to fracture is also studied. The results obtained show fracture toughness to be a function of laminate thickness, being in all cases independent of crack size. The fracture surface of all thick laminates was uniform in the interior and self-similar with the starter notch. With only one exception, the fracture toughness of the thicker laminates was relatively independent of specimen configuration. |
| NASA分類 | COMPOSITE MATERIALS |
| レポートNO | 86A41060 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/384042 |
|
