| タイトル | Compression of laminated composite beams with initial damage |
| 著者（英） | Breivik, Nicole L.; Gurdal, Zafer; Griffin, O. H., Jr. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1993-07-01 |
| 言語 | eng |
| 内容記述 | The effect of isolated damage modes on the compressive strength and failure characteristics of laminated composite test specimens were evaluated experimentally and numerically. In addition to specimens without initial damage, specimens with three types of initial damage were considered: (1) specimens with short delaminations distributed evenly through the specimen thickness, (2) specimens with few long delaminations, and (3) specimens with local fiber damage in the surface plies under the three-point bend contact point. It was found that specimens with short multiple delamination experienced the greatest reduction in compression strength compared to the undamaged specimens. Single delaminations far from the specimen surface had little effect on the final compression strength, and moderate strength reduction was observed for specimens with localized surface ply damage. |
| NASA分類 | STRUCTURAL MECHANICS |
| レポートNO | 93A44479 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/316437 |
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