Effect of an overload on the threshold level of Ti-6-22-22

ASTM Special Technical Publication

Volumn , Issue 1372, 2000, Pages 123-134

  McEvily, A J ^a   Ohashi, M ^b   Shover, R ^a   DeCarmine, A ^a  

^a UNIVERSITY OF CONNECTICUT   (United States)

^b NATIONAL RESEARCH INSTITUTE OF POLICE SCIENCE   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

CRACK PROPAGATION; FATIGUE TESTING; TITANIUM ALLOYS; YIELD STRESS;

FATIGUE THRESHOLD; OVERLOADS;

FATIGUE OF MATERIALS;

EID: 0033896942     PISSN: 10403094     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1520/stp13430s     Document Type: Conference Paper

References (6)

1. Lineberger, L., "Titanium Aerospace Alloy," Advanced Materials and Processes, ASM, Vol. 153, No.5, May 1998, pp. 45-46.
2. Stephens, R. R., Stephens, R. I., Veit, A. L. and Anderson, T. P., "Fatigue Crack Growth of Ti-62222 Titanium Alloy under Constant Amplitude and MiniTwist Flight Spectra at 25° C and 175°, Int. J. Fatigue, Vol. 19, 1997, pp. 301-308.
3. McEvily, A. J. and Yang, Z., "The Nature of the Two Opening Levels Following an Overload in Fatigue Crack Growth, Met. Trans, Vol. 21A, 1990, pp. 2717-27.
4. Bao, H. and McEvily, A. J., The Effect of an Overload on the Rate of Fatigue Crack Propagation under Plane Stress Conditions, Met. Trans., Vol. 26A, 1995, pp. 1725-33.
5. Paris, P. C. and Hermann, L., Fatigue Thresholds. J. Backlund, A. F. Blom, and C. J. Beevers, Eds., EMAS, Warley, UK, Vol. 1, 1985, p.11.
6. Phillips, E. P. and Newman, J. C., Jr., Private communication, 1998.