Charts are presented from which 24S-T (bare sheet) and 75S-T (Alclad sheet) aluminum alloy flat compression panels may be designed to have minimum weight required to carry given intensity of loading at given effective length of panel with given sheet thickness.


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    Title :

    Design charts for flat compression panels having longitudinal extruded Y-section stiffeners and comparison with panels having formed Z-section stiffeners


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Dow, N.F. (author) / Hickman, W.A. (author)


    Publication date :

    1947


    Size :

    41 pages


    Remarks:

    35 Supp sheets


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :