Variations in drag with taper ratio, aspect ratio, sweepback, and Mach number are determined; calculations are presented for families of tapered wings having equal root bending stress.


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    Title :

    Supersonic wave drag of sweptback tapered wings at zero lift


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1947


    Size :

    49 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :