Part of test program given is concerned with panels in which thickness of stiffener material is 0.625 times skin thickness; results show effect of relative dimensions of panel on buckling stress; comparative envelope curves for hat stiffened and Z-stiffened panels provide indication of relative structural efficiencies of two types of panel.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Compressive strength of 24S-T aluminum-alloy flat panels with longitudinal formed hat-section stiffeners


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1946


    Size :

    10 pages


    Remarks:

    12 Supp plates


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :