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    T-Tail Flutter Analysis with Simulated Fuselage Stiffness

    Source: Journal of Aerospace Engineering:;2015:;Volume ( 028 ):;issue: 006
    Author:
    Ju Qiu
    ,
    Qin Sun
    DOI: 10.1061/(ASCE)AS.1943-5525.0000328
    Publisher: American Society of Civil Engineers
    Abstract: The current work is a contribution to the potential effect of the aft fuselage stiffness modifications on the flutter characteristics of a T-tail. The rear fuselage is simulated by beam elements, based on a fixed T-tail structure. Their stiffness ranges from
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      T-Tail Flutter Analysis with Simulated Fuselage Stiffness

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    http://yetl.yabesh.ir/yetl1/handle/yetl/56479
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    contributor authorJu Qiu
    contributor authorQin Sun
    date accessioned2017-05-08T21:34:20Z
    date available2017-05-08T21:34:20Z
    date copyrightNovember 2015
    date issued2015
    identifier other%28asce%29as%2E1943-5525%2E0000330.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/56479
    description abstractThe current work is a contribution to the potential effect of the aft fuselage stiffness modifications on the flutter characteristics of a T-tail. The rear fuselage is simulated by beam elements, based on a fixed T-tail structure. Their stiffness ranges from
    publisherAmerican Society of Civil Engineers
    titleT-Tail Flutter Analysis with Simulated Fuselage Stiffness
    typeJournal Paper
    journal volume28
    journal issue6
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000328
    treeJournal of Aerospace Engineering:;2015:;Volume ( 028 ):;issue: 006
    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