Effect of stress ratio on fatigue crack growth in a titanium aluminide alloy
Bibliographic record
Abstract
No abstract is available for this record. The assistant can identify its topic from the title, but cannot infer the study’s results.
Source: Not provided · Quality: missing
Research context
OpenAlex topics: Intermetallics and Advanced Alloy Properties · Aluminum Alloys Composites Properties · Advanced Welding Techniques Analysis
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (6)
Show source-provided references
1. B.K. Parida and T. Nicholas, in Proceedings of International Conference on Fracture of Engineering Materials and Structures, S.H. Teoh and K.H. Lee (eds.), Elsevier Science Publishers, London (1991) 685–690.10.1007/978-94-011-3650-1_101 ↗
2. J.R. Jira, K.S. Ravichandran and J.M. Larsen, “Fatigue Crack Growth of Surface Flaws in Ti-24A1-11Nb”, paper presented at The Metallurgical Society of American Institute of Mining Engineers Symposium on Creep, Fatigue and Fracture of Titanium Aluminides, Indianapolis, 1–5 October 1989.
3. D.P. DeLuca, B.A. Cowles, F.K. Haake and K.P. Holland, in Fatigue and Fracture of Titanium Aluminides, Wright Reseach and Development Center Report No. TR-89-4136 (1990) 14–21.10.21236/ADA226737 ↗
4. K.S. Ravichandran and J.M. Larsen, in Fracture Mechanics, 22nd Symposium, ASTM STP 1149, H.A. Ernst, A. Saxena and McDowell (eds.) (1991) in press.
5. K. Walker, in Effects of Environment and Complex Load History on Fatigue Life, ASTM STP 462 (1970) 1–14.
6. K. Tanaka, in Fracture Mechanics Perspectives and Directions, ASTM STP 1020, R.P. Wei and R.P. Gangloff (eds.), (1989) 151–183.10.1520/STP18824S ↗