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    Titel :

    Reduced Order Modeling of Flow over a NACA 0015 Airfoil for Control Application (AIAA 2014-2516)



    Kongress:

    Conference; 7th, Flow control; 7th AIAA flow control conference 2014; Atlanta, Georgia, USA, 16-20 June 2014 : held at the AIAA aviation forum 2014 ; 2014 ; Atlanta, GA



    Erscheinungsdatum :

    01.01.2014


    Format / Umfang :

    18 pages


    Anmerkungen:

    Includes bibliographical references and index



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Reduced Order Modeling of Flow over a NACA 0015 Airfoil For Control Application

    Caraballo, Edgar J. / Sullivan, Taylor / Little, Jesse C. | AIAA | 2014


    Control of Separated Flow on a NACA 0015 Airfoil using Three-Dimensional Plasma Actuator (AIAA 2014-2665)

    Wong, C. / Wang, L. / Wu, Z. et al. | British Library Conference Proceedings | 2014


    Vortex Developments Over NACA 0015 Airfoil with Trailing Edge Jet

    Okong'o, N. / Finaish, F. / Society of Automotive Engineers | British Library Conference Proceedings | 1994



    Vortex Developments Over NACA 0015 Airfoil with Trailing Edge Jet

    Finaish, Fathi / Okong'o, Nora | SAE Technical Papers | 1994