Results cover extensive range of sweepback angle, Mach number, aspect ratio, and thickness ratio; results for total wave drag are applicable both to sweptback and sweptforward wings.


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    Title :

    Theoretical supersonic wave drag of untapered sweptback and rectangular wings at zero lift


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1947


    Size :

    43 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :