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    Stabilization of the Cyclic Response of the Ni49.9 Ti50.1 Shape Memory Actuators under Thermomechanical Loads

    Source: Journal of Aerospace Engineering:;2021:;Volume ( 034 ):;issue: 001::page 04020099
    Author:
    A. F. Saleeb
    ,
    M. A. Soudah
    ,
    J. S. Owusu-Danquah
    DOI: 10.1061/(ASCE)AS.1943-5525.0001211
    Publisher: ASCE
    Abstract: This 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.
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      Stabilization of the Cyclic Response of the Ni49.9 Ti50.1 Shape Memory Actuators under Thermomechanical Loads

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4269194
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    • Journal of Aerospace Engineering

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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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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian