Effect of step testing and notches on the endurance limit of Ti-6AI-4V

American Society of Mechanical Engineers, Materials Division (Publication) MD

Volumn 84, Issue , 1998, Pages 27-30

  Bellows, Richard S ^a   Bain, Ken R ^b   Sheldon, Jerry W ^c  

^a HONEYWELL   (United States)

^b GE AVIATION   (United States)

^c United Technologies   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CRACK INITIATION; DURABILITY; FATIGUE TESTING; PLASTICITY; RESIDUAL STRESSES; STRESS ANALYSIS;

STEP TESTING;

TITANIUM ALLOYS;

EID: 11544280693     PISSN: 10716939     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Article

References (3)

1. Cowles, B.A., 1996 "High Cycle Fatigue in Aircraft Gas Turbines - An Industry Perspective," International Journal of Fatigue, Vol. 80. pp. 147-163.
2. Nicholas. T. and J.R. Zuiker, 1996 "On the Use of the Goodman Diagram for High Cycle Fatigue Design," International journal of Fatigue, Vol. 80, pp. 219-235.
3. Sinclair, G. M., 1952, "An Investigation of the Coaxing Effect in Fatigue of Metals," ASTM Proceedings, Vol. 52,pp. 743-758.