Coefficients of lift, drag and pitching moment are given at zero yaw; coefficients of rolling moment, yawing moment, and side force given for rectangular wing at all values of yaw tested; results discussed.


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    Title :

    Wind-tunnel investigations of effect of yaw on lateral-stability characteristics. I: four N.A.C.A. 23012 wings of various plan forms with and without dihedral


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Bamber, M.J. (author) / House, R.O. (author)


    Publication date :

    1939


    Remarks:

    Supp sheets, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :