Research Article
SVR Prediction Algorithm for Crack Propagation of Aviation Aluminum Alloy
Table 6
Partial test data of constant amplitude two-hole test specimen 03.
| | | A | B | C | D |
| | 13000 | 0.6 | 0.9 | 0.9 | 0.9 | | 13200 | 0.6 | 0.9 | 0.9 | 1 | | 13400 | 0.7 | 1 | 1.1 | 1 | | 13600 | 0.8 | 1 | 1.1 | 1.05 | | 13800 | 0.8 | 1.2 | 1.2 | 1.05 | | … | | 18900 | 5 | 4.7 | 5 | 5.6 | | 18925 | 5.2 | 4.7 | 5 | 5.9 | | 18950 | 5.5 | 4.7 | 5 | 6.2 | | 18975 | 5.7 | 4.7 | 5 | 6.6 | | 19000 | 6 | 4.7 | 5 | 7 |
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