Stress is derived for simply supported panel in axial compression having stiffener offering no torsional restraint; results presented in form of curves and table; because panel of moderate or large curvature buckles in compression at stress considerably below theoretical value, method is suggested to aid in determining critical stress for use in design.


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    Titel :

    Critical axial-compressive stress of curved rectangular panel with Central chordwise stiffener


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Batdorf, S.B. (Autor:in) / Schildrcrout, M. (Autor:in)


    Erscheinungsdatum :

    1948


    Format / Umfang :

    23 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :