Data obtained in NACA full scale wind tunnel concerning effects of interference and of propeller operation on longitudinal stability and control have been studied; data include pitching moments for various power conditions for airplanes with tails removed and with tails set at various stabilizer and elevator angles; results are given for eight airplanes.


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    Title :

    Longitudinal stability and control with special reference to slipstream effects


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:
    Katzoff, S. (author)


    Publication date :

    1940


    Size :

    29 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :