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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    Titel :

    Analysis of low-aspect-ratio aircraft structures


    Weitere Titelangaben:

    J Aerospace Sciences


    Beteiligte:
    Samson, Jr., C.H. (Autor:in) / Bergmann, H. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1960


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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