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High temperature monotonic and cyclic deformation in a directionally solidified nickel-base superalloyDirectionally solidified (DS) MAR-M246+Hf was tested in tension and fatigue, at temperatures from 20 C to 1093 C. Tests were performed on (001) oriented specimens at strain rates of 50 % and 0.5 % per minute. In tension, the yield strength was constant up to 704 C, above which the strength dropped off rapidly. A strong dependence of strength on strain rate was seen at the higher temperatures. The deformation mode was observed to change from heterogeneous to homogeneous with increasing temperature. Low Cycle Fatigue tests were done using a fully reversed waveform and total strain control. For a given plastic strain range, lives increased with increasing temperature. For a given temperature strain rate had a strong effect on life. At 704 C, decreasing strain rates decreased life, while at the higher temperatures, decreasing strain rates increased life, for a given plastic strain range. These results could be explained through considerations of the deformation modes and stress levels. At the higher temperatures, marked coarsening caused beneficial stress reductions, but oxidation limited the life. The longitudinal grain boundaries were found to influence slip behavior. The degree of secondary slip adjacent to the boundaries was found to be related to the degree of misorientation between the grains.
Document ID
19870005870
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Huron, Eric S.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1986
Subject Category
Metallic Materials
Report/Patent Number
NAS 1.26:175101
USAAVSCOM-TR-86-C-19
NASA-CR-175101
AD-A171480
Report Number: NAS 1.26:175101
Report Number: USAAVSCOM-TR-86-C-19
Report Number: NASA-CR-175101
Report Number: AD-A171480
Accession Number
87N15303
Funding Number(s)
CONTRACT_GRANT: NAG3-503
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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