Weight of compression panel subjected to given buckling load investigated as function of stiffener spacing, plate thickness, and geometry of stiffener cross section; charts presented for determination of optimum stiffener spacing and plate thickness.


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    Title :

    Minimum-weight design of simply supported transversely stiffened plates under compression


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Gomza, A. (author) / Seide, P. (author)


    Publication date :

    1948


    Size :

    23 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English