EFFECT OF STEP TESTING AND NOTCHES ON THE ENDURANCE LIMIT OF Ti-6AI-4V

ASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE)

Volumn 1998-S, Issue , 1998, Pages 27-32

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

^a Allied Signal Engines   (United States)

^b GE AVIATION   (United States)

^c PRATT AND WHITNEY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; FATIGUE DAMAGE; FATIGUE TESTING; GAS TURBINES; SOFTWARE TESTING;

DAMAGE MODES; ENDURANCE LIMIT; FATIGUE BEHAVIOUR; NOTCH FATIGUE; NOTCH GEOMETRY; S-N CURVE; SINGLE SPECIMEN; STEP TEST; STRESS RATIO; TEST METHOD;

GEOMETRY;

EID: 85124383558     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/IMECE1998-1138     Document Type: Conference Paper

References (5)

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. Maxwell, D.C. and T. Nicholas, 1998 "A Rapid Method for Generation of a Haigh Diagram for High Cycle Fatigue," ASTM STP 1321, T.L. Panontin and S.D. Sheppard, Editors, to be published.
4. Sendeckyj, G.P. 1998 "History of Constant Life Diagrams," High Cycle Fatigue of Structural Materials, W.O. Soboyejo and T.S. Srivatsan, Editors, pp. 95-107.
5. Sinclair, G. M., 1952, "An Investigation of the Coaxing Effect in Fatigue of Metals," ASTM Proceedings, Vol. 52, pp. 743-758.