Derivation of empirical equation to fit experimental values of profile drag determined from N A C A tests on uniform-section rectangular airfoils at varying lift coefficients; determining profile drag of more general airfoil; induced drag is simplified and combined with profile drag to get complete expression for drag coefficient of tapered airfoil; relative merit of various planeforms.


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    Titel :

    Drag of tapered cantilever airfoils


    Weitere Titelangaben:

    Aeronautical Sciences -- J


    Beteiligte:
    Upson, R.H. (Autor:in) / Thompson, M.J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1934


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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