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    Titel :

    Aeroelasticity and Dynamic Analysis of Cracked Composite Wings Using Spectral Finite Element Method (AIAA 2014-0677)



    Kongress:

    Conference; 55th, AIAA/ASME/ASME/ASCE/AHS/SC Structures, structural dynamics and materials ; 2014 ; National Harbor, MD



    Erscheinungsdatum :

    2014-01-01


    Format / Umfang :

    13 pages


    Anmerkungen:

    Includes bibliographical references and author index



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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