The aerodynamic characteristics of three types of six-bladed main rotors are calculated on the basis of the nonlinear free vortex wake model. The vortex wake shapes and induced velocity fields in the rotors jet are analyzed. The figure of merit (FoM) diagrams are received.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Comparative Study of a Conventional, Coaxial Counter-Rotating, and Co-Rotating Rotor Aerodynamics in Hover


    Weitere Titelangaben:

    Russ. Aeronaut.


    Beteiligte:
    Makeev, P. V. (Autor:in) / Ignatkin, Yu. M. (Autor:in) / Shaidakov, V. I. (Autor:in) / Nikitin, S. O. (Autor:in)

    Erschienen in:

    Russian Aeronautics ; 64 , 2 ; 233-239


    Erscheinungsdatum :

    01.04.2021


    Format / Umfang :

    7 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Performance of a Mach-Scale Coaxial Counter-Rotating Rotor in Hover

    Cameron, Christopher G | Online Contents | 2016


    Performance of a Mach-Scale Coaxial Counter-Rotating Rotor in Hover

    Cameron, Christopher G | Online Contents | 2016


    Performance of a Mach-Scale Coaxial Counter-Rotating Rotor in Hover

    Cameron, Christopher G. / Karpatne, Anand / Sirohi, Jayant | AIAA | 2016


    Phase-Resolved Flowfield Measurements of a Coaxial Counter-Rotating Rotor in Hover

    Mortimer, Patrick / Sirohi, Jayant / Platzer, Stefan et al. | AIAA | 2023


    COAXIAL COUNTER-ROTATING ROTOR SYSTEM

    CORRIGAN JOHN / STAMPS FRANK B | Europäisches Patentamt | 2018

    Freier Zugriff