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    Flutter Control of Smart Composite Structures in Hygrothermal Environment

    Source: Journal of Aerospace Engineering:;2010:;Volume ( 023 ):;issue: 004
    Author:
    P. K. Mahato
    ,
    D. K. Maiti
    DOI: 10.1061/(ASCE)AS.1943-5525.0000046
    Publisher: American Society of Civil Engineers
    Abstract: Flutter control of smart composite plates under subsonic airflow is investigated in hygrothermal environment. The active fiber composite (AFC) which is more effective and adaptive than the conventional monolithic piezoelectric material is used in the present analysis to control the undesirable response due to hygrothermal effect. The velocity and displacement feedback control algorithm are subsequently established to reduce actively the response of the plate. Numerical examples of isotropic and laminated composite plates with or without hygrothermal effect are presented. It is observed that the structures become weak in the presence of hygrothermal load in the form of reduced flutter boundary. The flutter boundary can be enhanced with the help of AFC. The parametric study is performed and it is observed that the flutter boundary can be enhanced with the help of a feedback-control system activating the AFC. Therefore, one can say that the AFC is effective to enhance the flutter boundary of the present aeroelastic structure in the hygrothermal environment.
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      Flutter Control of Smart Composite Structures in Hygrothermal Environment

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    http://yetl.yabesh.ir/yetl1/handle/yetl/56185
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    contributor authorP. K. Mahato
    contributor authorD. K. Maiti
    date accessioned2017-05-08T21:33:40Z
    date available2017-05-08T21:33:40Z
    date copyrightOctober 2010
    date issued2010
    identifier other%28asce%29as%2E1943-5525%2E0000046.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/56185
    description abstractFlutter control of smart composite plates under subsonic airflow is investigated in hygrothermal environment. The active fiber composite (AFC) which is more effective and adaptive than the conventional monolithic piezoelectric material is used in the present analysis to control the undesirable response due to hygrothermal effect. The velocity and displacement feedback control algorithm are subsequently established to reduce actively the response of the plate. Numerical examples of isotropic and laminated composite plates with or without hygrothermal effect are presented. It is observed that the structures become weak in the presence of hygrothermal load in the form of reduced flutter boundary. The flutter boundary can be enhanced with the help of AFC. The parametric study is performed and it is observed that the flutter boundary can be enhanced with the help of a feedback-control system activating the AFC. Therefore, one can say that the AFC is effective to enhance the flutter boundary of the present aeroelastic structure in the hygrothermal environment.
    publisherAmerican Society of Civil Engineers
    titleFlutter Control of Smart Composite Structures in Hygrothermal Environment
    typeJournal Paper
    journal volume23
    journal issue4
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000046
    treeJournal of Aerospace Engineering:;2010:;Volume ( 023 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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