Computation of induced yawing moment which is said to be greatest part of entire yawing moment encountered by wings.


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    Title :

    A new relation between the induced yawing moment and the rolling moment of an airfoil in straight motion


    Additional title:

    U. S. Nat Advisory Comm. Aeronautics -- Report


    Contributors:
    Munk, M.M. (author)


    Publication date :

    1924


    Size :

    5 pages


    Remarks:

    1 Fig.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :