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Charpy Impact Energy and Microindentation Hardness of 60-NITINOL60-NITINOL (60 wt.% Ni 40 wt.% Ti) is being studied as a material for advanced aerospace components. The Charpy impact energy and microindentation hardness has been studied for this material, fabricated by vacuum induction skull melting (casting) and by hot isostatic pressing. Test specimens were prepared in various hardened and annealed heat treatment conditions. The average impact energy ranged from 0.33 to 0.49J for the hardened specimens while the annealed specimens had impact energies ranging from 0.89 to 1.18J. The average hardness values of the hardened specimens ranged from 590 to 676 HV while that of the annealed specimens ranged from 298 to 366 HV, suggesting an inverse relationship between impact energy and hardness. These results are expected to provide guidance in the selection of heat treatment processes for the design of mechanical components.
Document ID
20120016607
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Stanford, Malcolm K.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 26, 2013
Publication Date
September 1, 2012
Subject Category
Metals And Metallic Materials
Report/Patent Number
E-18333
NASA/TM-2012-216029
GRC-E-DAA-TN5435
Report Number: E-18333
Report Number: NASA/TM-2012-216029
Report Number: GRC-E-DAA-TN5435
Funding Number(s)
WBS: WBS 877868.02.07.03.01.03.04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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