2002
DOI: 10.1361/105994902770343593
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Influence of the Post-Deformation Annealing Heat Treatment on the Low-Cycle Fatigue of NiTi Shape Memory Alloys

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Cited by 27 publications
(48 citation statements)
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“…The elastic properties attributed to the resin-rich zone, sheath, and Ti-Ni SMA element are presented in Table 3. For this work, Young’s modulus of the Ti-Ni SMA wires (55 GPa) corresponds to a mean value between Young’s modulus of martensite (30 GPa) and austenite (80 GPa) phases (Brailovski et al, 2003). Preliminary calculations indicate that this simplification does not significantly affect the panel’s rigidity (with a discrepancy of less than 3%).…”
Section: Host Structurementioning
confidence: 99%
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“…The elastic properties attributed to the resin-rich zone, sheath, and Ti-Ni SMA element are presented in Table 3. For this work, Young’s modulus of the Ti-Ni SMA wires (55 GPa) corresponds to a mean value between Young’s modulus of martensite (30 GPa) and austenite (80 GPa) phases (Brailovski et al, 2003). Preliminary calculations indicate that this simplification does not significantly affect the panel’s rigidity (with a discrepancy of less than 3%).…”
Section: Host Structurementioning
confidence: 99%
“… ID: inner diameter; OD: outer diameter; SMA: shape memory alloy. a Huntsman resin data sheet. b Zeus sheath data sheet. c Brailovski et al (2003). …”
Section: Host Structurementioning
confidence: 99%
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“…Therefore, it is important to understand how the microstructure of the SMAs can be optimised to provide good fatigue behaviour. The process of improvement not only has to avoid the plastic deformation of the martensite phase, but also has to simultaneously obtain high yield strength in the austenite phase [7][8][9].…”
Section: Introductionmentioning
confidence: 99%