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    Membrane Micro Air Vehicles with Adaptive Aerodynamic Twist: Numerical Modeling

    Source: Journal of Aerospace Engineering:;2009:;Volume ( 022 ):;issue: 002
    Author:
    Bret Stanford
    ,
    Peter Ifju
    DOI: 10.1061/(ASCE)0893-1321(2009)22:2(173)
    Publisher: American Society of Civil Engineers
    Abstract: Micro air vehicles are typically characterized by a low aspect ratio wing operating at low Reynolds numbers
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      Membrane Micro Air Vehicles with Adaptive Aerodynamic Twist: Numerical Modeling

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    http://yetl.yabesh.ir/yetl1/handle/yetl/45158
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    contributor authorBret Stanford
    contributor authorPeter Ifju
    date accessioned2017-05-08T21:16:25Z
    date available2017-05-08T21:16:25Z
    date copyrightApril 2009
    date issued2009
    identifier other%28asce%290893-1321%282009%2922%3A2%28173%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/45158
    description abstractMicro air vehicles are typically characterized by a low aspect ratio wing operating at low Reynolds numbers
    publisherAmerican Society of Civil Engineers
    titleMembrane Micro Air Vehicles with Adaptive Aerodynamic Twist: Numerical Modeling
    typeJournal Paper
    journal volume22
    journal issue2
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(2009)22:2(173)
    treeJournal of Aerospace Engineering:;2009:;Volume ( 022 ):;issue: 002
    contenttypeFulltext
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