With reference to aircraft practice, formula for buckling under compression of flat rectangular plate stiffened only transversely is applied to design problem of determining least total weight of material necessary to support specified load; successive steps in process described with least possible reference to mathematical analysis. (See also - discussion pt 8 July/Aug p D175-8)


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    Title :

    Design of transversely stiffened flat plating


    Additional title:

    North-East Coast Instn Engrs Shipbldrs -- Trans


    Contributors:
    Cox, H.L. (author)


    Publication date :

    1950


    Size :

    14 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English







    Design of transversely loaded plating based on allowable permanent set

    Konieczny, L. / Bogdaniuk, M. | British Library Online Contents | 1999


    Interframe Buckling of Aluminum Alloy Stiffened Plating

    J. D. Clarke / J. W. Swan | NTIS | 1985