In this work, numerical studies are conducted for a supersonic M = 2.0 steady flow over a flat plate with a suction through single circular hole of variating intensity. The computed flow fields near the suction hole are estimated to build special boundary condition of Dirichlet type. Such a simulated suction can be used in DNS of disturbances propagation over walls with multiple suction holes.


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    Title :

    Modelling of suction for supersonic laminar flow control


    Contributors:

    Conference:

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


    Published in:

    Publication date :

    2021-05-24


    Size :

    11 pages





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English






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