Measurements were made at 0.50 Mach to determine the effects of sideslip angle and propeller operation on the tail-load distribution. It is shown that asymmetric tail loading results from a large decrease in load on the blanketed tail and a small increase of load on the leading tail. The asymmetric loads and torsional moments at low speeds and zero angle of sideslip are unimportant even during power-on conditions.


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    Title :

    Measurements of the Pressure Distribution on the Horizontal Tail Surface of a Typical Propeller-Driven Pursuit Airplane in Flight. 2 - The Effect of Angle of Sideslip and Propeller Operation


    Contributors:
    M. Sadoff (author) / L. A. Clousing (author)

    Publication date :

    1947


    Size :

    53 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English