The main objective is to develop effective control strategies for separation control of an airfoil with a single hinge flap. The specific objectives are: Develop an active control architecture for flow control around an airfoil with flap. Design, fabricate, a wind tunnel test of a high lift wing (with flap) with integrated actuators and sensors. Design, development and fabrication of synthetic jet actuators. Develop appropriate control strategy for application to the airfoil. Wind tunnel testing of the high lift wing at various angles of attack and flap positions with closed loop control.


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    Titel :

    Active Flow Control of Lifting Surface With Flap-Current Activities and Future Directions


    Beteiligte:
    Ahmadi, G. (Autor:in) / Marzocca, P. (Autor:in) / Jha, R. (Autor:in) / Alstorm, B. (Autor:in) / Obied, S. (Autor:in) / Kabir, P. (Autor:in) / Shahrabi, A. (Autor:in)


    Erscheinungsdatum :

    2010-02-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    ABS Transport Statistics: current activities and future directions

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    New directions in lifting surface theory

    ASHLEY, H. / LANDAHL, M. | AIAA | 1964


    New directions in lifting surface theory

    ASHLEY, H. / LANDAHL, M. T. / WINDALL, S. | AIAA | 1965


    Active Flow Control for Trailing Edge Flap Separation

    Pack Melton, LaTunia G. / Koklu, Mehti / Andino, Marlyn Y. et al. | AIAA | 2018