Combined experimental-numerical investigation of fretting fatigue crack initiation

International Journal of Fatigue

Volumn 23, Issue 8, 2001, Pages 703-711

  Lykins, Christopher D ^a   Mall, Shankar ^a   Jain, Vinod K ^b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b University of Dayton   (United States)

Author keywords

Fretting fatigue crack initiation; Titanium alloy

Indexed keywords

CORROSION FATIGUE; CRACK INITIATION; FINITE ELEMENT METHOD; FRETTING CORROSION; SHEAR STRESS; STRESS ANALYSIS;

SMITH-WATSON-TOPPER CRITICAL PLANE PARAMETER;

TITANIUM ALLOYS;

EID: 0035452323     PISSN: 01421123     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0142-1123(01)00029-9     Document Type: Article

References (19)

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5. Effects of contact pressure on fretting fatigue of high strength steel and titanium alloy. Standardization of fretting fatigue test methods and equipment
6. Effects of contact stress and slip distance on fretting fatigue damage in Ti-6A1-4V/17-4Ph contacts
7. Length scale considerations in fretting fatigue
8. Fundamental investigations of fretting fatigue
9. Analysis of contact pressure and stress amplitude effects on fretting fatigue life
10. An evaluation of parameters for predicting fretting fatigue crack initiation
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12. Effects of cyclic frequency and contact pressure on fretting fatigue under two-level block loading
13. The effect of stress ratio during crack propagation and fatigue for 2024-T3 and 7075-T6 aluminum. Effects of environment and complex load history on fatigue life
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15. A stress-strain function for the fatigue of metals
16. On the initiation of fretting fatigue cracks