Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Numerical Investigation of Active Flow Control on a Pitching NACA 0015 Airfoil using Detached-Eddy Simulation (AIAA 2014-0765)



    Kongress:

    52nd, Aerospace sciences meeting; held at the AIAA SciTech Forum 2014 ; 2014 ; National Harbor, MD



    Erscheinungsdatum :

    2014-01-01


    Format / Umfang :

    6 pages


    Anmerkungen:

    Includes bibliographical references and author index



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Detached-Eddy Simulation of Flow Past a Pitching NACA 0015 Airfoil with Pulsed Actuation (AIAA 2016-1832)

    Wang, Liang / Li, Liying / Fu, Song | British Library Conference Proceedings | 2016



    Effects of Synthetic Jet Actuation on a Pitching NACA 0015 Airfoil

    Traub, L. W. / Miller, A. C. / Redinitis, O. et al. | British Library Conference Proceedings | 2004


    Effects of Synthetic Jet Actuation on a Pitching NACA 0015 Airfoil

    Traub, Lance / Miller, Adam / Rediniotis, Othon | AIAA | 2004


    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