Two methods presented provide for arbitrary external loading, are general with respect to orientation of structural members, and permit arbitrary boundary conditions; consistent distortion method; transfer matrix method; application to rectangular and nonrectangular wings.


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    Title :

    Analysis of low-aspect-ratio aircraft structures


    Additional title:

    J Aerospace Sciences


    Contributors:

    Published in:

    Publication date :

    1960


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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