Abstract This chapter describes the possible application of Rod Vortex Generators (RVGs) on helicopter rotor blades. Two different flight conditions are considered: hover and forward flight. The numerical model is validated with the available experimental data of the Caradonna–Tung model helicopter rotor blade (hover conditions) and the AH-1G helicopter (forward flight conditions). The application of RVGs on both rotor blades leads to an increment of the thrust coefficient with a power consumption penalty


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Implementation of Rod Vortex Generators on Helicopter Rotor Blades in Hover and Forward Flight Conditions


    Beteiligte:
    Tejero, Fernando (Autor:in) / Doerffer, Piotr (Autor:in) / Flaszyński, Paweł (Autor:in) / Szulc, Oskar (Autor:in)


    Erscheinungsdatum :

    2017-01-01


    Format / Umfang :

    19 pages




    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    Field Measurements of Helicopter Rotor Wash in Hover and Forward Flight

    Teske, M. E. / Kaufman, A. E. / George, C. W. et al. | British Library Conference Proceedings | 1995


    Field Measurements of Helicopter Rotor Wash in Hover and Forward Flight

    Milton E. Teske / Andrew E. Kaufman / Charles W. George et al. | AIAA | 1997


    Numerical simulation of a helicopter rotor in hover and forward flight

    Webster, Robert / Chen, Jen / Whitfield, David | AIAA | 1995


    Field Measurements of Helicopter Rotor Wash in Hover and Forward Flight

    Teske, M. E. / Kaufman, A. E. / George, C. W. et al. | British Library Conference Proceedings | 1995