The nonlinear response and failure characteristics of internally pressurized 4- to 16-ply cylindrical panels of graphite/epoxy are experimentally and analytically studied. Tests simulated the skin of a typical transport aircraft fuselage under loading to eventual failure. Aluminum test specimens were similarly tested and compared. All graphite/epoxy panels are found to withstand the internal pressures applied, which are well above the proof pressure loading expected for transport fuselage structures.


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    Titel :

    Nonlinear response and failure characteristics of clamped internally pressurized graphite-epoxy cylindrical panels


    Beteiligte:

    Erscheinungsdatum :

    01.01.1984


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



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    Impact response of graphite/epoxy cylindrical panels

    PALAZOTTO, A. / PERRY, R. / SANDHU, R. | AIAA | 1992