Experimental work done by National Advisory Committee for Aeronautics on panels; resulting design charts developed for 24S-T aluminum alloy panels with formed Z section stiffeners and for 24S-T and 75S-T aluminum alloy panels with extruded Y-section stiffeners. (See also - discussion p 143-4)


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    Title :

    Design charts for longitudinally stiffened wing compression panels


    Additional title:

    Soc Automotive Engrs -- Trans


    Contributors:
    Dow, N.F. (author)


    Publication date :

    1949


    Size :

    21 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English






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