Load history effects on fatigue crack growth threshold for Ti-6Al-4V and Ti-17 titanium alloys

International Journal of Fatigue

Volumn 23, Issue SUPPL. 1, 2001, Pages 253-258

  Moshier, M A ^a   Nicholas, T ^a   Hillberry, B M ^b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b PURDUE UNIVERSITY   (United States)

Author keywords

Crack growth; Fatigue; Loading history; Overload; Threshold; Ti 17; Ti 6Al 4V; Titanium alloys

Indexed keywords

ANNEALING; CRACK PROPAGATION; FATIGUE OF MATERIALS; LOADS (FORCES); STRESSES;

HIGH CYCLE FATIGUE (HCF); LOADING HISTORY;

TITANIUM ALLOYS;

EID: 0035210928     PISSN: 01421123     EISSN: None     Source Type: Journal    
DOI: 10.1016/s0142-1123(01)00118-9     Document Type: Article

References (10)

1. Critical issues in high cycle fatigue
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4. Step test, stress ratio, and surface effects on the high cycle behavior of Ti-6Al-4V
5. On the definition of lower-bound fatigue-crack propagation thresholds in Ti-6Al-4V under high cycle fatigue conditions
6. Mixed-mode crack-growth thresholds in Ti-6Al-4V under turbine-engine high-cycle fatigue loading conditions
7. The growth of cracks in Ti-6Al-4V plate under combined high and low cycle fatigue
8. A rapid method for generation of a Haigh diagram for high cycle fatigue
9. Analysis of overload effects and related phenomena