| タイトル | A mixed-mode bending apparatus for delamination testing |
| 本文（外部サイト） | http://hdl.handle.net/2060/19890001574 |
| 著者（英） | Crews, John H., Jr.; Reeder, James R. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1988-08-01 |
| 言語 | eng |
| 内容記述 | A mixed-mode delamination test procedure was developed combining double cantilever beam mode I loading and end notch flexure mode II loading on a split unidirectional laminate. By loading the specimen with a lever, a single applied load simultaneously produces mode I and II bending loads on the specimen. This mixed mode bending (MMB) test was analyzed using both finite element procedures and beam theory to calculate the mode I and II components of strain energy release rate, G sub I and G sub II, respectively. The analyses showed that a wide range of G sub I/G sub II ratios could be produced by varying the applied load position on the loading lever. As the delamination extended, the G sub I/G sub II ratios varied by less than 5 percent. The simple beam theory equations were modified to account for the elastic interaction between the two arms of the specimen and to account for shear deformations. The resulting equations agreed closely with the finite element results and provide a basis for selection of G sub I/G sub II test ratios and a basis for computing the mode I and II components of measured delamination toughness. The MMB specimen analysis and test procedures were demonstrated using unidirectional laminates. |
| NASA分類 | COMPOSITE MATERIALS |
| レポートNO | 89N10945
NASA-TM-100662
NAS 1.15:100662 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/144970 |
