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    Titel :

    Effect of Plasma Actuators on a Flat Plate Laminar Boundary Layer in Subsonic Conditions



    Kongress:

    25th, Aerodynamic measurement technology and ground testing conference ; 2006 ; San Francisco, CA



    Erscheinungsdatum :

    01.01.2006


    Format / Umfang :

    AIAA Paper 2006-3350


    Anmerkungen:

    Including 25th AIAA aerodynamic measurement technology and ground testing conference 24th AIAA applied aerodynamics conference; 3rd AIAA flow control conference; 36th AIAA fluid dynamics conference and exhibit; 37th AIAA plasmadynamics and lasers conference; 9th AIAA/ASME joint thermophysics and heat transfer conference.; Paper numbers 2006-2805 to 2006-3925 with gaps held. Held on CD-ROM.; Shelved in Conference Index - see disc 11 for papers from the 25th Aerodynamic measurement technology and ground testing conference


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Effect of Plasma Actuators on a Flat Plate Laminar Boundary Layer in Subsonic Conditions

    Seraudie, Alain / Aubert, Eddy / Naudé, Nicolas et al. | AIAA | 2006




    STABILIZING A LAMINAR BOUNDARY-LAYER USING PLASMA-ACTUATORS

    Grundmann, S. / Klumpp, S. / Tropea, C. et al. | British Library Conference Proceedings | 2006


    Effect of Flat Plate Oscillation on Boundary Layer Development for Subsonic Flows

    Amir, M. / Kontis, K. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006