Influence of contact configuration on fretting fatigue behavior of Ti-6Al-4V under independent pad displacement condition

International Journal of Fatigue

Volumn 24, Issue 12, 2002, Pages 1243-1253

  Jin, O ^a   Mall, S ^b  

^a Air Force Institute of Technology   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

Contact mechanics; Fretting fatigue; Fretting wear; Slip amplitude; Titanium alloy

Indexed keywords

FATIGUE TESTING; MICROCRACKS; STRESSES;

FRETTING FATIGUE;

TITANIUM ALLOYS;

EID: 0036883759     PISSN: 01421123     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0142-1123(02)00041-5     Document Type: Article

References (19)

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15. Effect of independent pad displacement on fretting fatigue behavior of Ti-6Al-4V
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18. Influence of contact configuration in fretting fatigue testing
19. Analyses of contact pressure and stress amplitude effects on fretting fatigue life