Approximate relation derived for surface velocity potential of wings when they are contained within Mach cone from vortex; this relation is applied to obtain pressure distributions, lift and rag coefficients, center of pressure, and rolling moments as function of angle of yaw for delta wing.


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    Title :

    Effects of yawing thin pointed wings at supersonic speeds


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1947


    Size :

    17 pages


    Remarks:

    9 Supp sheets


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :