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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    Title :

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


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1947


    Size :

    34 pages


    Remarks:

    6 Supp Plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :