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    Finite Element Analysis of Aeroelasticity of Plates and Shells

    Source: Applied Mechanics Reviews:;1992:;volume( 045 ):;issue: 012::page 461
    Author:
    Maher N. Bismarck-Nasr
    DOI: 10.1115/1.3119783
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A review of the finite element method applied to the problem of supersonic aeroelastic stability of plates and shells is presented. The review is limited to linear models. Some new contributions in the field are presented and future trends are discussed.
    keyword(s): Aeroelasticity , Finite element analysis , Plates (structures) , Shells , Stability AND Finite element methods ,
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      Finite Element Analysis of Aeroelasticity of Plates and Shells

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    http://yetl.yabesh.ir/yetl1/handle/yetl/109549
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    contributor authorMaher N. Bismarck-Nasr
    date accessioned2017-05-08T23:37:15Z
    date available2017-05-08T23:37:15Z
    date copyrightDecember, 1992
    date issued1992
    identifier issn0003-6900
    identifier otherAMREAD-25636#461_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/109549
    description abstractA review of the finite element method applied to the problem of supersonic aeroelastic stability of plates and shells is presented. The review is limited to linear models. Some new contributions in the field are presented and future trends are discussed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleFinite Element Analysis of Aeroelasticity of Plates and Shells
    typeJournal Paper
    journal volume45
    journal issue12
    journal titleApplied Mechanics Reviews
    identifier doi10.1115/1.3119783
    journal fristpage461
    journal lastpage482
    identifier eissn0003-6900
    keywordsAeroelasticity
    keywordsFinite element analysis
    keywordsPlates (structures)
    keywordsShells
    keywordsStability AND Finite element methods
    treeApplied Mechanics Reviews:;1992:;volume( 045 ):;issue: 012
    contenttypeFulltext
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