Stiffened sheet panels are used frequently in aircraft as structural members carrying axial loads; full section compressive tests were made on short lengths of stiffeners of both alloys to determine relative strength of sections without any effect from sheet.


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    Title :

    Comparative tests on extruded 14s-T and extruded 24s-T hat-shape stiffener sections


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Holt, M. (author) / Feil, G.W. (author)


    Publication date :

    1947


    Size :

    8 pages


    Remarks:

    9 Supp plates


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :




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