Research Article
Competitive Failure of Loosening and Fatigue of Bolts under Composite Excitation
Table 1
Combinations of composite excitation in competitive failure tests.
| Transverse displacement amplitude (mm) | Axial load amplitude (kN) | ξ (mm/kN) | Number of valid specimens |
| 0.5 | 0 | — | 2 | 0.5 | 5 | 0.1 | 3 | 0.5 | 6 | 0.0833 | 3 | 0.5 | 8 | 0.0625 | 3 | 0.6 | 0 | — | 2 | 0.6 | 2 | 0.3 | 5 | 0.6 | 4 | 0.15 | 5 | 0.6 | 6 | 0.1 | 3 | 0.6 | 8 | 0.075 | 3 | 0.6 | 9.6 | 0.0625 | 3 | 0.6 | 10 | 0.06 | 3 | 0.7 | 0 | — | 3 | 0.7 | 2 | 0.35 | 3 | 0.7 | 5 | 0.14 | 3 | 0.7 | 7 | 0.1 | 3 | 0.7 | 8 | 0.0875 | 3 | 0.7 | 9 | 0.0778 | 3 | 0.7 | 11.2 | 0.0625 | 3 | 0.8 | 0 | — | 2 | 0.8 | 2 | 0.4 | 3 | 0.8 | 4 | 0.2 | 3 | 0.8 | 6 | 0.1333 | 3 | 0.8 | 8 | 0.1 | 3 | 0.8 | 10 | 0.08 | 3 | 0.8 | 12 | 0.0667 | 3 | 0.8 | 12.8 | 0.0625 | 3 | 0.9 | 0 | — | 3 | 0.9 | 2 | 0.45 | 3 | 0.9 | 4 | 0.225 | 3 | 0.9 | 6 | 0.15 | 3 | 0.9 | 9 | 0.1 | 3 | 0.9 | 14.4 | 0.0625 | 3 | 1.0 | 0 | — | 3 | 1.0 | 1 | 1 | 3 | 1.0 | 2 | 0.5 | 3 | 1.0 | 4 | 0.25 | 3 | 1.0 | 10 | 0.1 | 3 | 1.0 | 12 | 0.0833 | 2 | 0 | 12 | 0 | 1 |
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