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Material characterization of superplastically formed titanium (Ti-6Al-2Sn-4Zr-2Mo) sheetThe aerospace industry has focused considerable interest on the near-alpha titanium alloy Ti-6Al-2Sn-4Zr-2Mo (Ti-6242) because of both its high-temperature properties and its superplastic forming (SPF) capabilities. This paper describes current research to characterize selected mechanical properties of Ti-6242 sheet in the SPF-strained condition, both with and without heat treatment, and compares the results with those obtained on as-received material. Tensile and creep tests were conducted, and metallographic analysis was performed to show the effect of 100 to 700 percent SPF strain on titanium properties. Analysis shows that as a result of SPF processing, both tensile and yield strengths, as well as elongation, are moderately reduced. Creep tests at 800 F and 1000 F show that the SPF processed material displays superior creep resistance compared with the as-received material. A post-SPF duplex-anneal heat treatment had no beneficial effect on tensile and creep properties.
Document ID
19870010974
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Ossa, William A.
(PRC Kentron, Inc. Hampton, Va., United States)
Royster, Dick M.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1987
Subject Category
Metallic Materials
Report/Patent Number
NASA-TP-2674
NAS 1.60:2674
L-16115
Report Number: NASA-TP-2674
Report Number: NAS 1.60:2674
Report Number: L-16115
Accession Number
87N20407
Funding Number(s)
PROJECT: RTOP 505-43-43-06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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