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    Title :

    Two Stage Damage Tolerance Evaluation of an Aircraft Fuselage Panel with a Circumferential Crack and a Broken Stringer



    Conference:

    Conference; 54th, Structures, structural dynamics and materials; 54th AIAA/ASME/ASCE/AHS/ASC structures ; 2013 ; Boston, MA



    Publication date :

    2013-01-01


    Size :

    20 pages


    Remarks:

    Includes bibliographical references and index



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English







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