The new developed airplane structures present a collection of several technologies and materials. This tendency is based on the load tailored design of modern airplanes. Especially, the fuselage contains different affected areas. In consequence of the technology substitutions made, the effort of validation and approval activities grows significantly. So the role of curved panel tests has to be redefined. The capability of special task test devices has improved continuously. With the reached higher simulation accuracy the experimental fatigue and damage tolerance analysis has been enabled for the whole panel including every stiffener detail.


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    Titel :

    A test concept for future aircraft fuselage panels


    Beteiligte:
    Best, R. (Autor:in) / Fleischer, T. (Autor:in) / Götze, M. (Autor:in) / Sachse, M. (Autor:in) / Semsch, M. (Autor:in)


    Erscheinungsdatum :

    2009


    Format / Umfang :

    12 Seiten, 11 Bilder, 4 Quellen




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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