Acta Aeronautica et Astronautica Sinica ›› 2024, Vol. 45 ›› Issue (7): 228952.doi: 10.7527/S1000-6893.2023.28952
• Solid Mechanics and Vehicle Conceptual Design • Previous Articles Next Articles
Tongzhou GAO1, Xiaofan HE1, Xiaolei WANG2, Ziguang LI2, Zhentao ZHU2, Zhixin ZHAN1(
)
Received:2023-05-03
Revised:2023-05-22
Accepted:2023-06-07
Online:2024-04-15
Published:2023-06-09
Contact:
Zhixin ZHAN
E-mail:zzxupc@163.com
Supported by:CLC Number:
Tongzhou GAO, Xiaofan HE, Xiaolei WANG, Ziguang LI, Zhentao ZHU, Zhixin ZHAN. Fatigue life prediction of 2014-T6 aluminum alloy based on CDM theory and SVM model[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(7): 228952.
Table 5
Calculation results of fatigue life based on finite element numerical method of damage mechanics
| 数据编号 | Kt | R | 试验寿命/循环 | 预测寿命/ 循环 | 相对 误差/% | |
|---|---|---|---|---|---|---|
| 1 | 1 | -1 | 289.59 | 33 380 | 39 839 | 19.35 |
| 2 | 1 | -1 | 248.22 | 102 324 | 101 384 | -0.92 |
| 3 | 1 | -1 | 220.64 | 202 313 | 206 979 | 2.31 |
| 4 | 1 | -1 | 193.06 | 368 480 | 464 863 | 26.16 |
| 5 | 1 | -1 | 179.27 | 432 596 | 728 360 | 68.37 |
| 6 | 1 | -1 | 165.48 | 4 039 200 | 1 183 001 | -70.71 |
| 7 | 1 | 0 | 455.07 | 15 173 | 13 794 | -9.09 |
| 8 | 1 | 0 | 413.70 | 46 834 | 32 448 | -30.72 |
| 9 | 1 | 0 | 344.75 | 151 729 | 151 555 | -0.11 |
| 10 | 1 | 0 | 296.49 | 229 517 | 504 086 | 119.63 |
| 11 | 1 | 0 | 275.80 | 915 495 | 880 320 | -3.84 |
| 12 | 1 | 0.06 | 413.70 | 22 918 | 40 019 | 74.62 |
| 13 | 1 | 0.06 | 379.20 | 56 294 | 86 387 | 53.46 |
| 14 | 1 | 0.06 | 344.80 | 114 376 | 193 829 | 69.47 |
| 15 | 1 | 0.06 | 324.10 | 172 985 | 322 954 | 86.69 |
| 16 | 1 | 0.06 | 296.50 | 2 633 260 | 660 338 | -74.92 |
| 17 | 1 | 0.06 | 289.60 | 732 477 | 795 226 | 8.57 |
| 18 | 1 | 0.06 | 275.80 | 2 790 979 | 1 164 390 | -58.28 |
| 19 | 1 | 0.06 | 255.10 | 6 238 830 | 2 119 015 | -66.04 |
| 20 | 1.6 | -1 | 275.80 | 13 501 | 40 503 | 200.00 |
| 21 | 1.6 | -1 | 241.33 | 25 132 | 72 381 | 188.00 |
| 22 | 1.6 | -1 | 227.54 | 38 671 | 98 999 | 156.00 |
| 23 | 1.6 | -1 | 199.96 | 193 303 | 187 504 | -3.00 |
| 24 | 1.6 | -1 | 186.17 | 183 812 | 270 204 | 47.00 |
| 25 | 1.6 | -1 | 172.38 | 512 936 | 435 996 | -15.00 |
| 26 | 1.6 | -1 | 144.80 | 3 022 820 | 1 239 356 | -59.00 |
| 27 | 1.6 | -1 | 137.90 | 2 532 060 | 1 595 198 | -37.00 |
| 28 | 1.6 | -0.4 | 399.91 | 6 540 | 20 668 | 216.00 |
| 29 | 1.6 | -0.4 | 344.75 | 23 238 | 46 475 | 100.00 |
| 30 | 1.6 | -0.4 | 324.07 | 42 166 | 84 331 | 100.00 |
| 31 | 1.6 | -0.4 | 275.80 | 116 271 | 110 457 | -5.00 |
| 32 | 1.6 | -0.4 | 255.12 | 132 031 | 165 039 | 25.00 |
| 33 | 1.6 | -0.4 | 220.64 | 188 386 | 201 573 | 7.00 |
| 34 | 1.6 | -0.4 | 206.85 | 402 926 | 568 126 | 41.00 |
| 35 | 1.6 | -0.4 | 179.27 | 3 137 470 | 1 474 611 | -53.00 |
| 36 | 1.6 | 0.06 | 482.65 | 7 894 | 15 787 | 100.00 |
| 37 | 1.6 | 0.06 | 427.49 | 20 178 | 33 698 | 67.00 |
| 38 | 1.6 | 0.06 | 358.54 | 60 829 | 97 934 | 61.00 |
| 39 | 1.6 | 0.06 | 275.80 | 573 500 | 470 270 | -18.00 |
| 40 | 1.6 | 0.06 | 255.12 | 1 673 163 | 769 655 | -54.00 |
| 41 | 1.6 | 0.46 | 379.23 | 178 425 | 692 289 | 288.00 |
| 42 | 1.6 | 0.46 | 358.54 | 523 851 | 969 124 | 85.00 |
| 43 | 1.6 | 0.46 | 330.96 | 987 435 | 1 678 640 | 70.00 |
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