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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Effect of slipstream rotation in producing asymmetric forces on fuselage


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Ribner, H.S. (Autor:in) / MacLachlan, R. (Autor:in)


    Erscheinungsdatum :

    1947


    Format / Umfang :

    14 pages


    Anmerkungen:

    17 Supp plates


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    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