Fretting behavior of Ti-6Al-4V under combined high cycle and low cycle fatigue loading

International Journal of Fatigue

Volumn 23, Issue SUPPL. 1, 2001, Pages 455-461

  Namjoshi, S A ^a   Mall, S ^b  

^a AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

Cycle fatigue loading; Fretting; Ti 6Al 4V

Indexed keywords

FATIGUE OF MATERIALS; FATIGUE TESTING; STRUCTURAL LOADS; TURBINES;

HIGH CYCLE FATIGUE (HCF); LOW CYCLE FATIGUE (LCF);

TITANIUM ALLOYS;

EID: 0035214681     PISSN: 01421123     EISSN: None     Source Type: Journal    
DOI: 10.1016/s0142-1123(01)00143-8     Document Type: Article

References (16)

1. Fretting-fatigue: Current technologies and practices
2. A fretting-fatigue damage threshold concept
3. A critical review of fretting-fatigue investigations at the Royal Aerospace Establishment
4. Fretting-fatigue
5. An evaluation of parameters for predicting fretting-fatigue crack initiation
6. Improvement of high-temperature fretting fatigue strength by shot peening
7. Improving fretting fatigue strength at elevated temperatures by shot peening in steam turbine steel
8. Spectrum load effects on the fretting behavior of Ti-6Al-4V
9. Interaction of high-cycle and low-cycle fatigue on fretting-fatigue behavior of Ti-6AL-4V
10. Investigation of variable amplitude loading on fretting-fatigue behavior of Ti-6AL-4V
11. Effects of cycling frequency and contact pressure on fretting-fatigue under two-level block loading
12. The effect of stress ratio during crack propagation and fatigue for 2024-T3 and 7075-T6 aluminum
13. A shear based parameter for fretting-fatigue crack initiation
14. Analysis of contact pressure and stress amplitude effects on fretting-fatigue life