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Development of a Numerical Model for High-Temperature Shape Memory AlloysA thermomechanical hysteresis model for a high-temperature shape memory alloy (HTSMA) actuator material is presented. The model is capable of predicting strain output of a tensile-loaded HTSMA when excited by arbitrary temperature-stress inputs for the purpose of actuator and controls design. Common quasi-static generalized Preisach hysteresis models available in the literature require large sets of experimental data for model identification at a particular operating point, and substantially more data for multiple operating points. The novel algorithm introduced here proposes an alternate approach to Preisach methods that is better suited for research-stage alloys, such as recently-developed HTSMAs, for which a complete database is not yet available. A detailed description of the minor loop hysteresis model is presented in this paper, as well as a methodology for determination of model parameters. The model is then qualitatively evaluated with respect to well-established Preisach properties and against a set of low-temperature cycled loading data using a modified form of the one-dimensional Brinson constitutive equation. The computationally efficient algorithm demonstrates adherence to Preisach properties and excellent agreement to the validation data set.
Document ID
20060028493
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
DeCastro, Jonathan A.
(QSS Group, Inc. Cleveland, OH, United States)
Melcher, Kevin J.
(NASA Glenn Research Center Cleveland, OH, United States)
Noebe, Ronald D.
(NASA Glenn Research Center Cleveland, OH, United States)
Gaydosh, Darrell J.
(Ohio Aerospace Inst. Brook Park, OH, United States)
Date Acquired
September 7, 2013
Publication Date
July 1, 2006
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA/TM-2006-214356
E-15631
Funding Number(s)
WBS: WBS 581-02-01-03-07
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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