Source-sink method of R. T. JONES used to determine wave drag coefficients at zero angle of attack of family of unswept wings with diamond airfoil section; charts presented permit rapid determination of drag coefficient at any supersonic Mach number, aspect ratio, and taper.


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    Title :

    Effect of aspect ratio and taper on pressure drag at supersonic speeds of unswept wings at zero lift


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1947


    Size :

    22 pages


    Remarks:

    10 Supp Plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :