Wind tunnel tests were prompted by strong tendency of single engine fighter airplanes equipped with single rotating propeller to yaw toward left under conditions of high thrust and low speed; investigation made to check predictions for lateral force on fuselage alone.


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    Title :

    Effect of slipstream rotation in producing asymmetric forces on fuselage


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1947


    Size :

    14 pages


    Remarks:

    17 Supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Effect of Slipstream Rotation in Producing Asymmetric Forces on a Fuselage

    Maclachlan, Robert / Ribner, Herbert | NTRS | 1947


    Slipstream Rotation and Stability

    Stiesz, W. | Emerald Group Publishing | 1940



    PROPELLER SLIPSTREAM AND WING-FUSELAGE INTERFERENCE EFFECTS ON THREE-AXIS STABILITY AND CONTROL

    Renooij, M. / Slingerland, R. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2004