Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Effects of Burst Frequency and Momentum Coefficient of DBD Actuator on Control of Deep-stall Flow around NACA0015 at Re~c=2.6x10^5 (AIAA 2014-0766)


    Beteiligte:

    Kongress:

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



    Erscheinungsdatum :

    2014-01-01


    Format / Umfang :

    16 pages


    Anmerkungen:

    Includes bibliographical references and author index



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





    LES on Turbulent Separated Flow around NACA0015 at Reynolds Number 1,600,000 toward Active Flow Control (AIAA 2014-2687)

    Asada, K. / Sato, M. / Fujii, K. et al. | British Library Conference Proceedings | 2014


    Grid sensivity study for the turbulent viscous flow around a NACA0015 airfoil at stall

    Costes, M. / Royal Aeronautical Society | British Library Conference Proceedings | 2005


    Experimental Analysis of Burst Actuation for Separation Control around a Pitching NACA0015 Airfoil Using a DBD Plasma Actuator at Low Reynolds Number (AIAA 2018-1551)

    Sekimoto, Satoshi / Shimomura, Satoshi / Fukumoto, Hiroaki et al. | British Library Conference Proceedings | 2018


    Experimental Study on Delayed Feedback Flow Control around a NACA0015 Airfoil Using PSJA (AIAA 2017-0487)

    Ogawara, Kakuji / Nomoto, Masaaki / Taguchi, Yudai et al. | British Library Conference Proceedings | 2017