Fretting Fatigue Behavior of Cavitation Shotless Peened Ti–6Al–4V
✍ Scribed by Hyukjae Lee; Shankar Mall; Hitoshi Soyama
- Publisher
- Springer US
- Year
- 2009
- Tongue
- English
- Weight
- 468 KB
- Volume
- 36
- Category
- Article
- ISSN
- 1023-8883
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📜 SIMILAR VOLUMES
Relaxation behavior of residual stress in a shot-peened titanium alloy, Ti-6Al-4V subjected to fretting fatigue was investigated at room and elevated temperatures. Constant amplitude fretting fatigue tests were conducted at several maximum stress levels, σ max ranging from 333 to 666 MPa with a stre
## Abstract Low‐cycle‐fatigue texts in vacuum and air were performed. Under cyclic loading the Ti‐6Al‐4V showed both cyclic hardening and cyclic softening depending on heat treatment, stress amplitude, and microstructure. Plastic deformation of the β‐phase in the unaged condition due to stress indu