The concepts of flow vectoring have long been established through the use of mechanical moving surfaces such as ailerons, elevators, flaps, etc. to redirect the local flow on an aircraft in order to obtain high-lift control and thrust-vectoring. Only recently has aerodynamic flow vectoring been investigated whereby the flow may be redirected without any movable surfaces. The present study has addressed the open loop control of a wake by means of trailing edge suction to enhance, or introduce any asymmetry of the mean flow of the wake to produce aerodynamic flow vectoring.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Aerodynamic Flow Vectoring of Wakes


    Beteiligte:
    L. G. Redekopp (Autor:in)

    Erscheinungsdatum :

    1994


    Format / Umfang :

    5 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Global dynamics and flow vectoring in asymmetric wakes

    Hammond, D. / Redekopp, L. | AIAA | 1994


    Global Dynamics and Flow Vectoring in Asymmetric Wakes

    Hammond, D. / Redekopp, L. G. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 1994


    Aerodynamic Flow Control Using Jet Vectoring Plasma Actuators

    Ozturk, Ceren / Jacob, Jamey | AIAA | 2009


    Aerodynamic Flow Control Using Jet Vectoring Plasma Actuators

    Ozturk, C. / Jacob, J. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2009


    Aerodynamic thrust vectoring of jets

    Hammond, D / Lim, D / Redekopp, L | AIAA | 1995