Method employed in trials on rigid airship; results indicate that turning radius compares favorably with that for other large airships, that radius is independent of speed, that position of point of zero yaw is nearly independent of rudder angle and air speed, and that theoretical relation between radius and angle of yaw in turn is close approximation to actuality.


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    Title :

    Full-scale turning characteristics of the U.S. Los Angeles


    Additional title:

    Nat. Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1929


    Size :

    14 pages


    Remarks:

    8 Figs.


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :