The aerodynamical constants of an airplane necessary for the discussion of stability are partly observed and partly calculated. Among the calculated coefficients is n(p), which is the variation of yawing moment due to rolling. (author)


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    Title :

    The Variation of Yawing Moment Due to Rolling


    Contributors:

    Publication date :

    1918-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English