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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    Title :

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


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1948


    Size :

    23 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :