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    Titel :

    Gradient-Based Optimization of Postbuckled, Steered-Fiber Aircraft Shell Using Equivalent Static Loads (AIAA 2016-1967)


    Beteiligte:

    Kongress:

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



    Erscheinungsdatum :

    2016-01-01


    Format / Umfang :

    17 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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