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Yield Behavior of Solution Treated and Aged Ti-6Al-4VPost yield uniaxial tension-compression tests were run on a solution treated and aged (STA), titanium 6-percent aluminum 4-percent vanadium (Ti-6Al-4V) alloy to determine the yield behavior on load reversal. The material exhibits plastic behavior almost immediately on load reversal implying a strong Bauschinger effect. The resultant stress-strain data was compared to a 1D mechanics model and a finite element model used to design a composite overwrapped pressure vessel (COPV). Although the models and experimental data compare well for the initial loading and unloading in the tensile regime, agreement is lost in the compressive regime due to the Bauschinger effect and the assumption of perfect plasticity. The test data presented here are being used to develop more accurate cyclic hardening constitutive models for future finite element design analysis of COPVs.
Document ID
20140011332
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Ring, Andrew J.
(Ohio Aerospace Inst. Brook Park, OH, United States)
Baker, Eric H.
(Connecticut Reserve Technologies, Inc. Cleveland, OH, United States)
Salem, Jonathan A.
(Connecticut Reserve Technologies, Inc. Cleveland, OH, United States)
Thesken, John C.
(Connecticut Reserve Technologies, Inc. Cleveland, OH, United States)
Date Acquired
September 3, 2014
Publication Date
June 1, 2014
Subject Category
Air Transportation And Safety
Report/Patent Number
NASA/TM-2014-218322
GRC-E-DAA-TN11730
E-18921
Report Number: NASA/TM-2014-218322
Report Number: GRC-E-DAA-TN11730
Report Number: E-18921
Funding Number(s)
WBS: WBS 346620.01.13.01.01.01
CONTRACT_GRANT: NNC12BA01B
CONTRACT_GRANT: NNC07TA82T
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Strain
Fatigue
Load
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