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    How the Airfoil Shape of a Morphing Wing Is Actuated and Controlled in a Smart Way

    Source: Journal of Aerospace Engineering:;2015:;Volume ( 028 ):;issue: 001
    Author:
    T. L. Grigorie
    ,
    R. M. Botez
    ,
    A. V. Popov
    DOI: 10.1061/(ASCE)AS.1943-5525.0000372
    Publisher: American Society of Civil Engineers
    Abstract: This paper presents a smart way to actuate and control the airfoil shape of a morphing wing in the open-loop architecture. The actuation system uses smart material actuators such as shape memory alloys, disposed in two parallel actuation lines, and its control is performed with a Mamdani-type fuzzy logic proportional derivative (PD) controller. The morphing wing project description, its actuation system structure, and the control design and validation are highlighted in this paper. The results obtained by both numerical simulation and experimental validation (bench tests and wind-tunnel tests) are presented as part of the control design and validation. An analysis of the wind flow characteristics, based on the information provided by the pressure sensors mounted on the flexible skin of the morphing wing in the wind-tunnel tests, is included as a supplementary validation; the transition between laminar and turbulent flows is real-time visualized, and the aerodynamic efficiency of the controlled morphing wing is evaluated.
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      How the Airfoil Shape of a Morphing Wing Is Actuated and Controlled in a Smart Way

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    https://yetl.yabesh.ir/yetl1/handle/yetl/56517
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    contributor authorT. L. Grigorie
    contributor authorR. M. Botez
    contributor authorA. V. Popov
    date accessioned2017-05-08T21:34:33Z
    date available2017-05-08T21:34:33Z
    date copyrightJanuary 2015
    date issued2015
    identifier other%28asce%29as%2E1943-5525%2E0000374.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/56517
    description abstractThis paper presents a smart way to actuate and control the airfoil shape of a morphing wing in the open-loop architecture. The actuation system uses smart material actuators such as shape memory alloys, disposed in two parallel actuation lines, and its control is performed with a Mamdani-type fuzzy logic proportional derivative (PD) controller. The morphing wing project description, its actuation system structure, and the control design and validation are highlighted in this paper. The results obtained by both numerical simulation and experimental validation (bench tests and wind-tunnel tests) are presented as part of the control design and validation. An analysis of the wind flow characteristics, based on the information provided by the pressure sensors mounted on the flexible skin of the morphing wing in the wind-tunnel tests, is included as a supplementary validation; the transition between laminar and turbulent flows is real-time visualized, and the aerodynamic efficiency of the controlled morphing wing is evaluated.
    publisherAmerican Society of Civil Engineers
    titleHow the Airfoil Shape of a Morphing Wing Is Actuated and Controlled in a Smart Way
    typeJournal Paper
    journal volume28
    journal issue1
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000372
    treeJournal of Aerospace Engineering:;2015:;Volume ( 028 ):;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