Abstract The buckling and post-buckling behavior of curved cylindrical stringer-stiffened laminated composite and metal panels had been investigated both numerically and experimentally. The results were compared to those of cylindrical stringer-stiffened laminated composite shells to yield a way of determining the optimal structure to be used for axial compression loading. For the present tested structures, the composite panels showed the best load-weight ratio.


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    Title :

    Behavior of curved laminated composite panels and shells under axial compression


    Contributors:

    Published in:

    Publication date :

    2015-05-29


    Size :

    33 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English