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    Titel :

    Aircraft Tire Spin-Up Wear Analysis through Experimental Testing and Computational Modeling (AIAA 2016-0413)


    Beteiligte:

    Kongress:

    AIAA/ASCE/AHS/ASC Structures, structural dynamics and materials (Conference)



    Erscheinungsdatum :

    01.01.2016


    Format / Umfang :

    17 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch



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