Study relating to missile components with particular reference to plates having aspect ratios a/b for values equal to or greater than 1 or equal to or less than 4.


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    Title :

    Critical buckling stresses of simply supported flat rectangular plates under combined longitudinal compression, transverse compression, and shear


    Additional title:

    J Aeronautical Sciences


    Contributors:


    Publication date :

    1954


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :