Mutual interference between rotors, wing, and tail of helicopter has large effect upon overall performance and stability of aircraft; equations are developed for all three induced velocity components at arbitrary point and for arbitrary harmonic of vorticity distribution.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Equations for induced velocities near lifting rotor with nonuniform azimuthwise vorticity distribution


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Heyson, H.H. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    25 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Induced velocities near a lifting rotor with nonuniform disk loading

    Heyson, Harry H. / Katzoff, S. | TIBKAT | 1957



    Charts of induced velocities near lifting rotor

    Jewel, Jr., J.W. / Heyson, H.H. | Engineering Index Backfile | 1959


    Rotor Wake Computing With Lifting Lines and Vorticity Confinement

    Wenren, Y. / Steinhoff, J. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2009