Wind-tunnel data on the effect of small-scale stationary flow perturbation on laminar boundary-layer separation in the aft part of a body of revolution are presented. The experimental results obtained at low subsonic velocities through hot-wire measurements support an idea of controlling axisymmetric flow separation locally as it was found earlier in plane configurations on airfoils and wings.


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    Titel :

    Perturbed laminar flow separating from an axisymmetric body


    Beteiligte:
    Zanin, B. Yu. (Autor:in) / Dovgal, A. V. (Autor:in) / Sorokin, A. M. (Autor:in) / Fomin, Vasily (Herausgeber:in) / Shiplyuk, Alexander (Herausgeber:in)

    Kongress:

    INTERNATIONAL CONFERENCE ON THE METHODS OF AEROPHYSICAL RESEARCH (ICMAR 2020) ; 2020 ; Novosibirsk, Russia


    Erschienen in:

    Erscheinungsdatum :

    24.05.2021


    Format / Umfang :

    4 pages





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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