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Viscoelastic Response of the Titanium Alloy Ti-6-4: Experimental Identification of Time- and Rate-Dependent Reversible and Irreversible Deformation RegionsIn support of an effort on damage prognosis, the viscoelastic behavior of Ti-6Al-4V (Ti-6-4) was investigated. This report documents the experimental characterization of this titanium alloy. Various uniaxial tests were conducted to low load levels over the temperature range of 20 to 538 C to define tensile, creep, and relaxation behavior. A range of strain rates (6x10(exp -7) to 0.001/s) were used to document rate effects. All tests were designed to include an unloading portion, followed by a hold time at temperature to allow recovery to occur either at zero stress or strain. The titanium alloy was found to exhibit viscoelastic behavior below the "yield" point and over the entire range of temperatures (although at lower temperatures the magnitude is extremely small). These experimental data will be used for future characterization of a viscoelastic model.
Document ID
20140008853
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Lerch, Bradley A.
(NASA Glenn Research Center Cleveland, OH United States)
Arnold, Steven M.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
July 9, 2014
Publication Date
April 1, 2014
Subject Category
Metals And Metallic Materials
Aeronautics (General)
Report/Patent Number
NASA/TM-2014-216584
GRC-E-DAA-TN10455
E-18786
Funding Number(s)
WBS: WBS 534723.02.05.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
stress relaxation
modulus of elasticity
deformation
Titanium alloys
recovery
yield point
loading rate
creep tests
viscoelasticity
experimental results
temperature dependence
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