The German Bürgernahes Flugzeug (Citizen-Oriented Airplane) research program advances technologies for high-lift systems using circulation control Coandă-type flaps. The interaction of these high-lift systems with a propeller engine is the subject of the present work. A large and complex wind-tunnel model equipped with an active high-lift system and a powered propeller was designed, manufactured and instrumented. The wind-tunnel data show the potentials of the active high-lift system in three-dimensional wing applications. The results characterize and quantify the interactions between a propeller and a high-lift wing by using systematic variations of blowing momentum and propeller thrust. The results represent a unique database for future efforts to improve the efficiency of active lift and for validation of numerical simulation methods.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Aerodynamic Effects of Propeller Slipstream on a Wing with Circulation Control


    Beteiligte:
    Beck, Nils (Autor:in) / Radespiel, Rolf (Autor:in) / Lenfers, Carsten (Autor:in) / Friedrichs, Jens (Autor:in) / Rezaeian, Alireza (Autor:in)

    Erschienen in:

    Journal of Aircraft ; 52 , 5 ; 1422-1436


    Erscheinungsdatum :

    01.09.2015




    Medientyp :

    Aufsatz (Konferenz) , Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    Aerodynamic Effects of Propeller Slipstream on a Wing with Circulation Control by Internally Blown Flaps (AIAA 2014-0407)

    Beck, N. / Radespiel, R. / Lenfers, C. et al. | British Library Conference Proceedings | 2014


    Simulated propeller slipstream effects on a supercritical wing

    Welge, H. R. / Crowder, J. P. | NTRS | 1978



    Analysis of Propeller Slipstream Effects on a Trailing Wing

    Veldhuis, L. L. M. | British Library Online Contents | 1996