A computer program implements a finite-element-based method of predicting the deformations of thin aerospace structures made of isotropic materials or anisotropic fiber-reinforced composite materials. The technique and corresponding software are applicable to thin shell structures in general and are particularly useful for analysis of thin beamlike members having open cross-sections (e.g. I-beams and C-channels) in which significant warping can occur.


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    Title :

    Better Finite-Element Analysis of Composite Shell Structures


    Contributors:


    Publication date :

    2007-05-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English






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