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contributor authorA. F. Saleeb
contributor authorM. A. Soudah
contributor authorJ. S. Owusu-Danquah
date accessioned2022-01-30T22:34:31Z
date available2022-01-30T22:34:31Z
date issued1/1/2021
identifier other(ASCE)AS.1943-5525.0001211.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4269194
description abstractThis work is focused on the development of a novel strategy to achieve dimensional stability for 55NiTi actuators that operate at a relatively higher temperature; i.e., with an austenite finish temperature, Af, greater than 90°C. The key ingredient in this is to place the actuators in a state of significant deformations before the thermal cycling. Correspondingly, this will provide increased-stiffness regions purely due to kinematic/geometric nonlinearity effects. In turn, this effectively counteracts the tendency for cyclic evolutionary behavior inherent in the commercial NiTi material. To demonstrate the success of the new approach, modeling results are presented involving different actuators having various shapes, i.e., beams, disks, and rings, which are operating for many repeated thermal cycles under different bias load conditions, such as concentrated point force, ring line load, or distributed surface tractions.
publisherASCE
titleStabilization of the Cyclic Response of the Ni49.9 Ti50.1 Shape Memory Actuators under Thermomechanical Loads
typeJournal Paper
journal volume34
journal issue1
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)AS.1943-5525.0001211
journal fristpage04020099
journal lastpage04020099-15
page15
treeJournal of Aerospace Engineering:;2021:;Volume ( 034 ):;issue: 001
contenttypeFulltext


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