On basis of recently developed theory for finite sweptback wings at supersonic speeds, calculations of supersonic wave drag at zero lift were made for series of wings having thin symmetrical biconvex sections with untapered plan forms and various angles of sweepback and aspect ratios.


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    Titel :

    Calculations of supersonic wave drag of nonlifting wings with arbitrary sweepback and aspect ratio wings swept behind Mach lines


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Harmon, S.M. (Autor:in) / Swanson, M.D. (Autor:in)


    Erscheinungsdatum :

    1947


    Format / Umfang :

    34 pages


    Anmerkungen:

    6 Supp Plates


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :