Measurements of helicopter rotor wake flow were made at low advance ratio. Both steady and nonsteady data were taken in the wake using 3-D hot-film anemometry. Emphasis was placed on the presentation of the data. Motion pictures were obtained from the computer plots of the experimental velocity data.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Rotor flow research in low speed helicopter flight


    Additional title:

    Untersuchung der Stroemung an Rotorblaettern von Hubschraubern bei niedrigen Fluggeschwindigkeiten


    Contributors:

    Published in:

    Publication date :

    1981


    Size :

    24 Seiten


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English





    Helicopter flight control with variable rotor speed and torque limiting

    Guo, Wei / Horn, Joseph F. | Tema Archive | 2009


    Helicopter Flight Control with Variable Rotor Speed and Torque Limiting

    Guo, W. / Horn, J. / AHS International | British Library Conference Proceedings | 2009



    MULTIDISCIPLINARY COMPUTATIONAL ROTOR NOISE PREDICTION FOR HELICOPTER ROTOR IN HIGH-SPEED FORWARD FLIGHT

    Liu, Y. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011