An investigation is conducted of the importance of anisotropic terms in the design of composite corrugated panels, for a range of axial compressive load intensities. The two panel configurations treated were panels with tailored laminates and panels with a continuous laminate; both are of interest to aircraft designers and prone to anisotropic effects which are of as-yet undetermined extent. The importance of the anisotropic terms is measured by the difference between the design load and the buckling load obtained from the ultimate structural analysis.


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    Titel :

    Importance of anisotropy on design of compression-loaded composite corrugated panels


    Beteiligte:
    Gurdal, Zafer (Autor:in) / Young, Richard D. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.04.1990



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :