This article documents the development of synthetic jet actuator array hardware to augment high-lift system effectiveness in a wind tunnel model. The study involved the design, manufacture and bench test of a synthetic jet actuator array based on an inclined actuator configuration to reduce volume installation requirements without a loss in jet velocity relative to a non-inclined baseline model; incorporation of proper synthetic jet actuator systems wiring and internal synthetic jet actuator chamber pressure-sensing for actuator health monitoring. The peak velocity obtained from the inclined synthetic jet actuator array was 100 m/s, which favourably compares to the baseline array (∼90 m/s), while reducing the usable depth requirements by 50%. The final outcome of this study has been to apply the design lessons learned to develop a methodology for designing a synthetic jet actuator array with the constraints of using piezoelectric-based actuator technology for flow separation control applications.


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    Titel :

    Development of design methodology for a synthetic jet actuator array for flow separation control applications


    Beteiligte:
    Jabbal, Mark (Autor:in) / Liddle, Stephen (Autor:in) / Potts, Jonathan (Autor:in) / Crowther, William (Autor:in)


    Erscheinungsdatum :

    2013-01-01


    Format / Umfang :

    15 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Unbekannt






    2012-3242 Development of Design Methodology for Synthetic Jet Actuator Array for Flow Separation Control Applications

    Jabbal, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012


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    Weigel, Perez / Schüller, Martin / Gratias, André et al. | Springer Verlag | 2020

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    Bauer, Karin D. / Karch, Christian / Heilmann, Alexander et al. | AIAA | 2017