Influence of residual stresses on high cycle fatigue strength of Ti-6Al-4V subjected to foreign object damage

International Journal of Fatigue

Volumn 23, Issue SUPPL. 1, 2001, Pages 405-412

  Thompson, Steven R ^a   Ruschau, John J ^b   Nicholas, Theodore ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b UNIVERSITY OF DAYTON RESEARCH INSTITUTE   (United States)

Author keywords

Fatigue; Foreign object damage; Impact; Notch; Residual stress; Ti 6Al 4V

Indexed keywords

AIRFOILS; LOADING; RESIDUAL STRESSES; STRENGTH OF MATERIALS; TENSILE STRESS;

FOREIGN OBJECT DAMAGE (FOD);

FATIGUE OF MATERIALS;

EID: 0035213227     PISSN: 01421123     EISSN: None     Source Type: Journal    
DOI: 10.1016/s0142-1123(01)00166-9     Document Type: Article

References (23)

1. Critical issues in high cycle fatigue
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4. Influence of foreign object damage (FOD) on fatigue life of Simulated Ti-6Al-4V Airfoils
5. Compressor blade FOD in-service, its simulation and the effect of artificial FOD on HCF resistance
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7. Determining a true material fatigue crack growth threshold
8. A rapid method for generation of a Haigh diagram for high cycle fatigue
9. Evolution and effects of damage in Ti-6Al-4V under high cycle fatigue
10. Validation of the step test method for generating Haigh diagrams for Ti-6Al-4V
11. Effect of step testing and notches on the endurance limit of Ti-6Al-4V
12. Notch size effects in HCF behavior of Ti-6Al-4V
13. Notch sensitivity
14. Stress concentration factors, relating theoretical and practical factors in fatigue loading
15. Effects of ballistic impact damage on fatigue crack initiation in Ti-6Al-4V simulated engine blades
16. Fatigue crack growth rate characteristics of laser shock peened titanium