Submitted:
14 April 2025
Posted:
15 April 2025
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Abstract
Keywords:
1. Introduction
2. Materials and Methods
2.1. Dataset
- Amplitude stress tensor in multiaxial loading. Amplitude of normal and shear components of stress during cyclic multiaxial loading conditions.
- Mean stress tensor in multiaxial loading. Mean or average values of normal and shear components of stress during cyclic multiaxial loading conditions.
- Fatigue limit tensile stress in repeated uniaxial loading. Maximum stress that the material undergoes alternating cycles of stress with magnitudes in tension higher than compression.
- Fatigue limit stress in fully reversed uniaxial loading. Maximum stress that the material undergoes alternating cycles of stress with equal magnitudes in tension and compression.
- Torsion fatigue limit in repeated uniaxial loading. Maximum stress that the material undergoes alternating cycles of stress with the magnitudes in tension higher than compression.
- Torsion fatigue limit in fully reversed uniaxial loading. Maximum stress that the material undergoes alternating cycles of stress with equal magnitudes in tension and compression.
- Maximum (Ultimate) strength. Refers to the maximum stress or force that a material can withstand before undergoing fracture or failure.
- Yield strength. Denotes the stress or force at which a material begins to deform plastically without undergoing permanent deformation.
- Shifted phased in stress load. Different starting point of stress cycles with a or a phase shift compared to the original loading conditions.
2.1. Augmenting the Database
2.2. Model Training and Data Processing
2.3. Artificial Neural Network
3. Results
4. Discussion
5. Conclusions
Appendix A
References
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| No. | Tensile Stress Amplitude | Tensile Mean Stress | Shear Stress amplitude | Shear Mean Stress | Transformation matrix | |||||||||||
| xx | yy | zz | xx | yy | zz | xy | xz | yz | xy | xz | yz | |||||
| 1 | 417 | 510 | 209 | 90 | Original data point | |||||||||||
| 2 | 417 | 510 | -209 | 90 | ||||||||||||
| 3 | 417 | 510 | 209 | 90 | ||||||||||||
| 4 | 417 | 510 | -209 | 90 | ||||||||||||
| No. | Tensile Stress amplitude | Tensile Mean Stress | Shear Stress amplitude | Shear Mean Stress | ||||||||||||
| xx | yy | zz | xx | yy | zz | xy | xz | yz | xy | xz | yz | |||||
| 1 | 866 | 541 | 1060 | 822 | 417 | 510 | 209 | |||||||||
| 5 | 866* | |||||||||||||||
| 6 | 866† | |||||||||||||||
| 7 | 866† | |||||||||||||||
| 8 | 541* | |||||||||||||||
| 9 | 541† | |||||||||||||||
| 10 | 541† | |||||||||||||||
| 11 | 530* | 530* | ||||||||||||||
| 12 | 530† | 530† | ||||||||||||||
| 13 | 530† | 530† | ||||||||||||||
| 14 | 411* | 411* | ||||||||||||||
| 15 | 411† | 411† | ||||||||||||||
| 16 | 411† | 411† | ||||||||||||||
| Model | Fatigue prediction error (%) | |||
| Max | Min | Mean | Standard deviation | |
| Original FatLim | 11.700 | -18.277 | -0.183 | 3.202 |
| Expanded FatLim | 22.769 | -26.909 | -0.149 | 4.585 |
| Model | Fatigue prediction error (%) | |||
| Max | Min | Mean | Standard deviation | |
| Original FatLim | 15.09 | -15.94 | 0.95 | 5.41 |
| Expanded FatLim | 9.84 | -16.17 | 0.31 | 4.83 |
| Model | Fatigue prediction error (%) | |||
| Max | Min | Mean | Standard deviation | |
| Original FatLim | 5.79×106 | -1.00×102 | 2.44×105 | 8.35×105 |
| Expanded FatLim | 19.21 | -23.81 | -0.37 | 5.73 |
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