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Fatigue crack growth and low cycle fatigue of two nickel base superalloysThe fatigue crack growth and low cycle fatigue behavior of two P/M superalloys, Rene 95 and Astroloy, in the hot isostatically pressed (HIP) condition, was determined. Test variables included frequency, temperature, environment, and hold times at peak tensile loads (or strains). Crack initiation sites were identified in both alloys. Crack growth rates were shown to increase in argon with decreasing frequency or with the imposition of hold times. This behavior was attributed to the effect of oxygen in the argon. Auger analyses were performed on oxide films formed in argon. Low cycle fatigue lives also were degraded by tensile hold, contrary to previous reports in the literature. The role of environment in low cycle fatigue behavior is discussed.
Document ID
19840002200
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Stoloff, N. S.
(Rensselaer Polytechnic Inst. Troy, NY, United States)
Duquette, D. J.
(Rensselaer Polytechnic Inst. Troy, NY, United States)
Choe, S. J.
(Rensselaer Polytechnic Inst. Troy, NY, United States)
Golwalkar, S.
(Rensselaer Polytechnic Inst. Troy, NY, United States)
Date Acquired
September 4, 2013
Publication Date
September 16, 1983
Subject Category
Metallic Materials
Report/Patent Number
NASA-CR-174534
NAS 1.26:174534
Report Number: NASA-CR-174534
Report Number: NAS 1.26:174534
Accession Number
84N10267
Funding Number(s)
CONTRACT_GRANT: NAG3-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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