An investigation was conducted to provide general information on the magnitudes and directions of the aerodynamic forces and moments exerted on a model of a fighter airplane in spinning attitudes as measured on a rotary balance installed in the Langley 20-foot free- spinning tunnel. The investigation included the determination of the effect on the aerodynamic forces and moments of reversing the rudder, of modifying the tail, and of deflecting the flaps and lowering the landing gear.


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    Title :

    Aerodynamic Forces and Moments on a 1/10-Scale Model of a Fighter Airplane in Spinning Attitudes as Measured on a Rotary Balance in the Langley 20-Foot Free-Spinning Tunnel


    Contributors:
    R. W. Stone (author) / S. M. Burk (author) / W. J. Bihrle (author)

    Publication date :

    1950


    Size :

    52 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English