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Volumn 80, Issue 2, 1989, Pages 237-255

An assessment of the role of near-threshold crack growth in high-cycle-fatigue life prediction of aerospace titanium alloys under turbine engine spectra

(4) Larsen, J M a Worth, B D b Annis, C G c Haake, F K c

a AIR FORCE RESEARCH LABORATORY (United States)

b UNIVERSITY OF DAYTON RESEARCH INSTITUTE (United States)

c PRATT AND WHITNEY (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; CRACK PROPAGATION; ENGINES; FATIGUE; TURBINES-GAS;

EID: 0030439748 PISSN: 03769429 EISSN: 15732673 Source Type: Journal
DOI: 10.1007/BF00012671 Document Type: Article

Times cited : (57)

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