Curves obtained show total increase in weight of optimum designed sheet stiffener compression panel when skin thickness is increased by arbitrary amount; curves are based on data from tests conducted by NACA on 75S-T Y-stiffened panels; method may also be applied to plotting of other sheet stiffener compression panel data.


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    Titel :

    Effect of torsional stiffness requirements on wing structural weight


    Weitere Titelangaben:

    J Aeronautical Sciences


    Beteiligte:
    Micks, W.R. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1950


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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