dc.contributor.author | Atlı, K. C. | |
dc.contributor.author | Karaman, I. | |
dc.contributor.author | Noebe, R. D. | |
dc.contributor.author | Bigelow, G. | |
dc.contributor.author | Gaydosh, D. | |
dc.date.accessioned | 2019-10-21T21:12:23Z | |
dc.date.available | 2019-10-21T21:12:23Z | |
dc.date.issued | 2015 | |
dc.identifier.issn | 0964-1726 | |
dc.identifier.issn | 1361-665X | |
dc.identifier.uri | https://dx.doi.org/10.1088/0964-1726/24/12/125023 | |
dc.identifier.uri | https://hdl.handle.net/11421/21359 | |
dc.description | WOS: 000366111500024 | en_US |
dc.description.abstract | The 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.sponsorship | NASA 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.sponsorship | This 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.iso | eng | en_US |
dc.publisher | IOP Publishing LTD | en_US |
dc.relation.isversionof | 10.1088/0964-1726/24/12/125023 | en_US |
dc.rights | info:eu-repo/semantics/closedAccess | en_US |
dc.subject | High Temperature Shape Memory Alloys | en_US |
dc.subject | Martensitic Transformation | en_US |
dc.subject | Two-Way Shape Memory Effect | en_US |
dc.subject | Work Output | en_US |
dc.subject | Thermomechanical Training | en_US |
dc.title | Work production using the two-way shape memory effect in NiTi and a Ni-rich NiTiHf high-temperature shape memory alloy | en_US |
dc.type | article | en_US |
dc.relation.journal | Smart Materials and Structures | en_US |
dc.contributor.department | Anadolu Üniversitesi, Mühendislik Fakültesi, Makine Mühendisliği Bölümü | en_US |
dc.identifier.volume | 24 | en_US |
dc.identifier.issue | 12 | en_US |
dc.relation.publicationcategory | Makale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı | en_US |