A penalty model of synthetic micro-jet actuator with application to the control of wake flows

Creators: Pasquetti, Richard; Peres, Noele

Others:: Laboratoire Jean Alexandre Dieudonné (JAD) ; Université Nice Sophia Antipolis (1965 - 2019) (UNS) ; COMUE Université Côte d'Azur (2015-2019) (COMUE UCA)-COMUE Université Côte d'Azur (2015-2019) (COMUE UCA)-Centre National de la Recherche Scientifique (CNRS)-Université Côte d'Azur (UCA); Control, Analysis and Simulations for TOkamak Research (CASTOR) ; Inria Sophia Antipolis - Méditerranée (CRISAM) ; Institut National de Recherche en Informatique et en Automatique (Inria)-Institut National de Recherche en Informatique et en Automatique (Inria)-Laboratoire Jean Alexandre Dieudonné (JAD) ; Université Nice Sophia Antipolis (1965 - 2019) (UNS) ; COMUE Université Côte d'Azur (2015-2019) (COMUE UCA)-COMUE Université Côte d'Azur (2015-2019) (COMUE UCA)-Centre National de la Recherche Scientifique (CNRS)-Université Côte d'Azur (UCA)-Université Nice Sophia Antipolis (1965 - 2019) (UNS) ; COMUE Université Côte d'Azur (2015-2019) (COMUE UCA)-COMUE Université Côte d'Azur (2015-2019) (COMUE UCA)-Centre National de la Recherche Scientifique (CNRS)-Université Côte d'Azur (UCA)

Description

A simple model of synthetic (zero-net mass-flux) micro-jet is proposed and implemented in a large-eddysimulation spectral solver of the incompressible Navier–Stokes equations. Essentially, it is simplyrequired to introduce a penalty like term in the momentum equation, with a variable penalty coefficientthat culminates during the expulsion phase. Examples of applications are considered for the control ofseveral turbulent wake flows, the backward facing step, the D-shaped body and the square backAhmed body.

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A penalty model of synthetic micro-jet actuator with application to the control of wake flows

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Abstract

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