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    Title :

    Testing and Analysis of a Composite Non-Cylindrical Aircraft Fuselage Structure, Part I: Ultimate Design Loads (AIAA 2016-2176)


    Contributors:

    Conference:

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



    Publication date :

    2016-01-01


    Size :

    28 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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