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Effect of grain orientation and coating on thermal fatigue resistance of a directionally solidified superalloy (MAR-M 247)The effect of off-axis directionally solidified (DS) grain growth on thermal fatigue life of Mar-M 247 alloy was evaluated. Uncoated conventionally cast as well as DS wedge bars were cycled in a burner rig between 1070 C and room temperature. The longitudinal axis and leading edge of the specimen coincided. As the angle between the specimen longitudinal axis and growth axis increased, the thermal fatigue life decreased for both the uncoated and aluminide-coated bars. Life increases of about 50 cycles for the DS conditions were attributed to coating. The decrease in thermal fatigue life with increasing angle is primarily attributed to the increase in modulus of elasticity with increasing angle and not to the intersection of DS grain boundaries with the specimen leading edge. The thermal fatigue cracks were observed to be transgranular in the DS material. Limited tensile and stress-rupture properties of conventionally cast and off-axis DS Mar-M 247 alloy are also presented.
Document ID
19790014394
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bizon, P. T.
(NASA Lewis Research Center Cleveland, OH, United States)
Dreshfield, R. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Calfo, F. D.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1979
Subject Category
Structural Mechanics
Report/Patent Number
E-9968
NASA-TM-79129
Report Number: E-9968
Report Number: NASA-TM-79129
Accession Number
79N22565
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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