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dc.contributor.authorAtlı, K. C.
dc.contributor.authorKaraman, I.
dc.contributor.authorNoebe, R. D.
dc.contributor.authorBigelow, G.
dc.contributor.authorGaydosh, D.
dc.date.accessioned2019-10-21T21:12:23Z
dc.date.available2019-10-21T21:12:23Z
dc.date.issued2015
dc.identifier.issn0964-1726
dc.identifier.issn1361-665X
dc.identifier.urihttps://dx.doi.org/10.1088/0964-1726/24/12/125023
dc.identifier.urihttps://hdl.handle.net/11421/21359
dc.descriptionWOS: 000366111500024en_US
dc.description.abstractThe work output capacity of the two-way shape memory effect (TWSME) in a Ni50.3Ti29.7Hf20 (at%) high-temperature shape memory alloy (HTSMA) was investigated and compared to that of binary Ni49.9Ti50.1 (at%). TWSME was induced through a training procedure of 100 thermomechanical cycles under different tensile stresses. It was observed that TWSME in as-extruded and trained Ni50.3Ti29.7Hf20 could produce 0.7% strain against a compressive stress of 100 MPa, corresponding to a maximum work output of 0.08 J g(-1), compared to a maximum value of 0.06 J g(-1) for binary NiTi. A peak aging heat treatment of 3 h at 550 degrees C, which previously has been shown to result in near-perfect functional stability in Ni50.3Ti29.7Hf20 during isobaric thermal cycling, did not improve the TWSME and actually resulted in a decrease in the magnitude and stability of the TWSME and its work output capacity. Nevertheless, the magnitude of TWSM behavior of Ni50.3Ti29.7Hf20, in the absence of an aging heat treatment, renders it an attractive candidate for high-temperature TWSM actuation.en_US
dc.description.sponsorshipNASA Fundamental Aeronautics Program, Subsonic Fixed Wing project [NNX07AB56A]; FAP Aeronautical Sciences Project; TAC Transformational Tools & Technologies Project, Discipline Lead, Dale Hopkins; US Air Force Office of Scientific Research [FA9550-15-0287]en_US
dc.description.sponsorshipThis study was originally supported by the NASA Fundamental Aeronautics Program, Subsonic Fixed Wing project through Cooperative Agreement no. NNX07AB56A, with additional support from the FAP Aeronautical Sciences Project and the TAC Transformational Tools & Technologies Project, Discipline Lead, Dale Hopkins. The work performed at Texas A&M University was supported by the US Air Force Office of Scientific Research, under grant no. FA9550-15-0287. The authors wish to thank the Shape Memory Alloy Group at NASA Glenn Research Center for helpful discussions.en_US
dc.language.isoengen_US
dc.publisherIOP Publishing LTDen_US
dc.relation.isversionof10.1088/0964-1726/24/12/125023en_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectHigh Temperature Shape Memory Alloysen_US
dc.subjectMartensitic Transformationen_US
dc.subjectTwo-Way Shape Memory Effecten_US
dc.subjectWork Outputen_US
dc.subjectThermomechanical Trainingen_US
dc.titleWork production using the two-way shape memory effect in NiTi and a Ni-rich NiTiHf high-temperature shape memory alloyen_US
dc.typearticleen_US
dc.relation.journalSmart Materials and Structuresen_US
dc.contributor.departmentAnadolu Üniversitesi, Mühendislik Fakültesi, Makine Mühendisliği Bölümüen_US
dc.identifier.volume24en_US
dc.identifier.issue12en_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US


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