This graduation report presents an analytical model for the disc edge vortices behind the helicopter main rotor. The model has been developed to come to a better understanding of the formation of these vortices and to be able to simulate their influence on helicopter behavior during low speed flight. The model represents a first step into the direction of a more general model, capable of predicting the influence of main rotor/tail rotor interaction on helicopter stability and control.


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    Titel :

    Main Rotor Disc Edge Vortices: An Analytical Model


    Beteiligte:
    J. P. Roos (Autor:in)

    Erscheinungsdatum :

    1996


    Format / Umfang :

    83 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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