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Fatigue Behavior of a Third Generation PM Disk SuperalloyThe fatigue behavior of a 3rd generation PM disk alloy, LSHR, was studied at 1300 F. Tensile, creep, and fatigue tests were run on smooth and notched (Kt = 2) bars under a variety of conditions. Analysis of smooth bar fatigue data, run under strain and load control with R ratios of 0 and -1, showed that a stress based Smith-Watson-Topper approach could collapse the data set. While the tensile and creep data showed substantial notch strengthening at 1300 F, the fatigue data showed a life deficit for the notch specimens. A viscoplastic finite element model, which accounted for stress relaxation at the notch tip, provided the best correlation between the notched and smooth bar behavior, although the fatigue data was not fully rationalized based on this simplified viscoplastic model of the stresses at the notch tip.Inclusion of a 90 sec dwell at peak load was found to dramatically decrease notch fatigue life. This result was shown to be consistent with a simple linear creep-fatigue damage rule, where creep damage dominated at low stresses and fatigue damage was more prevalent at higher stresses.
Document ID
20080045886
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Gayda, John
(NASA Glenn Research Center Cleveland, OH, United States)
Gabb, Timothy P.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
October 1, 2008
Subject Category
Metals And Metallic Materials
Report/Patent Number
NASA/TM-2008-215462
E-16655
Report Number: NASA/TM-2008-215462
Report Number: E-16655
Funding Number(s)
WBS: WBS 598259.02.07.03.04.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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