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The Effect of Stabilization Heat Treatments on the Tensile and Creep Behavior of an Advanced Nickel-Based Disk AlloyAs part of NASA s Advanced Subsonic Technology Program, a study of stabilization heat treatment options for an advanced nickel-base disk alloy, ME 209, was performed. Using a simple, physically based approach, the effect of stabilization heat treatments on tensile and creep properties was analyzed in this paper. Solutions temperature, solution cooling rate, and stabilization temperature/time were found to have a significant impact on tensile and creep properties. These effects were readily quantified using the following methodology. First, the effect of solution cooling rate was assessed to determine its impact on a given property. The as-cooled property was then modified by using two multiplicative factors which assess the impact of solution temperature and stabilization parameters. Comparison of experimental data with predicted values showed this physically based analysis produced good results that rivaled the statistical analysis employed, which required numerous changes in the form of the regression equation depending on the property and temperature in question. As this physically based analysis uses the data for input, it should be noted that predictions which attempt to extrapolate beyond the bounds of the data must be viewed with skepticism. Future work aimed at expanding the range of the stabilization/aging parameters explored in this study would be highly desirable, especially at the higher solution cooling rates.
Document ID
20030063949
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Gayda, John
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
June 1, 2003
Subject Category
Metals And Metallic Materials
Report/Patent Number
E-13948
NASA/TM-2003-212372
NAS 1.15:212372
Report Number: E-13948
Report Number: NASA/TM-2003-212372
Report Number: NAS 1.15:212372
Funding Number(s)
WORK_UNIT: WU 522-83-32
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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