A simple 2D boundary element analysis, suitable for developing cost effective models for tapered composite laminates, is presented. Constant stress and displacement elements are used. Closed-form fundamental solutions are derived. Numerical results are provided for several configurations to illustrate the accuracy of the model.


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    Title :

    Simple boundary element analysis of laminated composite structures


    Contributors:
    Makeev, A. (author) / Armanios, E.A. (author)


    Publication date :

    2001


    Size :

    10 Seiten, 9 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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