A significant amount of research was devoted to understanding the mechanism of dynamic stall delay as applicable to the flow environment of a helicopter rotor in forward flight. One aspect of such research deals with the unsteady characteristics of two-dimensional airfoil sections over a Mach number range from 0.3 to 9.6, since such characteristics can be meaningfully related to rotor performance and loads. This paper summarizes the results of several oscillatory tests carried out on conventional, transonic and BLC-equipped airfoils.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Observations on the dynamic stall characteristics of advanced helicopter rotor airfoils


    Beteiligte:
    Dadone, L. (Autor:in)


    Erscheinungsdatum :

    01.01.1978


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Investigations of dynamic stall and dynamic stall control on helicopter airfoils

    Gardner, Anthony D. / Technische Universität Clausthal | TIBKAT | 2015

    Freier Zugriff

    Investigations of dynamic stall and dynamic stall control on helicopter airfoils

    Gardner, Anthony D. / Technische Universität Clausthal | TIBKAT | 2016



    Modern Testing Approaches Used to Characterize Dynamic Stall Regimes on Helicopter Airfoils

    Davidson, Phillip / Naughton, Jonathan / Sitaraman, Jaynarayanan | British Library Conference Proceedings | 2015


    HELICOPTER ROTOR BLADE STALL DETECTOR

    L VOV NIKOLAJ LEONIDOVICH / KHABAROV STANISLAV SERGEEVICH / NOSOV ANDREJ ANATOL EVICH et al. | Europäisches Patentamt | 2015

    Freier Zugriff