| タイトル | Fatigue-crack initiation and growth in notched 2024-T3 specimens monitored by a video tape system |
| 本文（外部サイト） | http://hdl.handle.net/2060/19760023517 |
| 著者（英） | Sova, J. A.; Crews, J. H., Jr.; Exton, R. J. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1976-08-01 |
| 言語 | eng |
| 内容記述 | Fatigue-crack initiation and early stages of growth in notched 2024-T3 aluminum alloy sheet specimens were monitored during constant-amplitude fatigue tests conducted for a range of stress ratios. A video tape system was developed to detect fatigue cracks 0.1 mm in length on the sheet surface and to monitor their growth. Fatigue cracks initiated either at the notch corner or on the notch surface. Most of the first fatigue cracks started as notch-corner cracks, and the crack-initiation period was defined as the number of cycles for which the crack was 0.1 mm in length on the sheet surface. For each of the stress ratios used, the results showed that at the low stress levels, the crack-initiation period constituted at least 90 percent of the fatigue lives. However, for the negative stress ratios at the high stress levels, cracks started as early as at about 40 percent of the fatigue lives. |
| NASA分類 | STRUCTURAL MECHANICS |
| レポートNO | 76N30605
L-10754
NASA-TN-D-8224 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/184744 |
