As will be evident again and again in this book, AoA has a direct influence on the actuator nonlinearities. Figure 2.1 shows an airfoil at two different angles; the yellow colored airfoil represents a situation under low AoA, and the red color one indicates a situation under high AoA. The characteristics of the SJA under these situations is different because the ambient flow separates from the surface closer to the leading edge as the AoA increases. As a result the affect of SJAs on the ambient flow is different in the two cases. The resultant lift and drag forces are also distinct.


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    Titel :

    Synthetic Jet Actuators and Arrays: Modeling and Control


    Weitere Titelangaben:

    Studies in Systems, Decision and Control


    Beteiligte:
    Deb, Dipankar (Autor:in) / Burkholder, Jason (Autor:in) / Tao, Gang (Autor:in)


    Erscheinungsdatum :

    23.07.2021


    Format / Umfang :

    31 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    ON THE COMPUTATIONAL MODELING OF SYNTHETIC JET ACTUATORS

    Bercovici, M. / Arad, E. / Seifert, A. et al. | British Library Conference Proceedings | 2006


    Aerodynamic Flow Control Using Synthetic Jet Actuators

    Amitay, Michael / Glezer, Ari | Tema Archiv | 2006


    Flow Control Using Plasma Actuators and Linear/Annular Plasma Synthetic Jet Actuators

    Santhanakrishnan, A. / Jacob, J. / Suzen, Y. et al. | British Library Conference Proceedings | 2006


    Flow Control Using Plasma Actuators and Linear/Annular Plasma Synthetic Jet Actuators

    Santhanakrishnan, Arvind / Jacob, Jamey / Suzen, Yildirim | AIAA | 2006