Results of tests under combined axial load and normal pressure made on 29 24S-T aluminum alloy sheet-stringer panels, for use in construction of airplane wings, pressurized cabins and hull bottoms.


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    Title :

    Effect of normal pressure on strength of axially loaded sheet-stringer panels


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    McPherson, A.E. (author) / Levy, S. (author) / Zibritosky, G. (author)


    Publication date :

    1946


    Size :

    21 pages


    Remarks:

    29 Supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Effect of normal pressure on strength of axially loaded sheet-stringer panels

    MacPherson, A. E. / Levy, Samuel / Zibritosky, George | TIBKAT | 1945


    Effect of Normal Pressure on Strength of Axially Loaded Sheet-stringer Panels

    Mcpherson, A E / Levy, Samuel / Zibritosky, George | NTRS | 1946


    Effect of curvature on strength of axially loaded sheet-stringer panels

    Ramerg, Walter / Levy, Samuel / Fienup, Kenneth L. | TIBKAT | 1944


    Effect of Curvature on Strength of Axially Loaded Sheet-stringer Panels

    Ramberg, Walter / Levy, Samuel / Fienup, Kenneth L | NTRS | 1944