Column and Plate Compressive Strengths of Aircraft Structural Materials -- Extruded 24S-T Aluminum Alloy, (Originally issued as Advance Restricted Report L5F08b)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Column and plate compressive strengths of aircraft structural materials -- Extruded 24s-T aluminum alloy


    Additional title:

    Nat Advisory Committee Aeronautics -- Wartime Report


    Contributors:
    Heimerl, G.J. (author) / Roy, J.A. (author)


    Publication date :

    1945


    Size :

    11 pages


    Remarks:

    12 Supp Plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English