Effect of Stress Ratio on Fatigue Crack Growth Behavior of Ti-6Al-2Zr-1Mo-1V Alloy
The fatigue crack growth behaviors of Ti-6.5Al-2Zr-1Mo-1V titanium alloy at different positive stress ratios (<i>R</i> = 0.1, 0.3 and 0.5) were investigated at room temperature. The effects of stress ratio <i>R</i> on the fatigue crack growth rates and fractures morphology we...
| Main Authors: | , |
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| Format: | Article |
| Language: | zho |
| Published: |
Journal of Aeronautical Materials
2018-06-01
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| Series: | Journal of Aeronautical Materials |
| Subjects: | |
| Online Access: | http://jam.biam.ac.cn/CN/Y2018/V38/I3/72 |