Data presented for 9 complete models, 20 fuselage shapes, and 3 wing models; author finds it necessary to place considerable reliance on past design experience in proportioning airplane so as to obtain reasonable degree of directional stability.


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    Title :

    Estimation of rate of change of yawing moment with sideslip


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Imlay, F.H. (author)


    Publication date :

    1938


    Size :

    8 pages


    Remarks:

    9 Supp sheets, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :