Optimum design analyses, carried out by Lockheed Missiles and Space Co, are presented for 8 types of ring supported cylinders; experimental results included for rectangular ring stiffened shells demonstrate validity of analyses; optimum configurations are calculated by minimum weight analysis, and information presented for design of either optimum or nonoptimum configurations.


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    Title :

    Optimum ring stiffened cylinders subjected to uniform hydrostatic pressure


    Additional title:

    SAE -- Paper


    Contributors:

    Conference:

    SAE Meeting ; 1962 Design



    Publication date :

    1962


    Size :

    11 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English