Compression tests on five stiffened N8 aluminium alloy plates covering typical full scale warship scantlings are described. The panels were manufactured using normal shipyard production methods to ensure typical initial distortion and residual stresses. Maximum loads and post-buckling load/deflection results are compared with theoretical predictions using the ARE computer program N106C. Keywords: Buckling, Strength, Test, Compression, Stiffened plate, Interframe, Yield.


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    Title :

    Interframe Buckling of Aluminum Alloy Stiffened Plating


    Contributors:
    J. D. Clarke (author) / J. W. Swan (author)

    Publication date :

    1985


    Size :

    68 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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