Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Control of Separated Boundary Layer by Means of Micro- Actuated Delta Wings



    Kongress:

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



    Erscheinungsdatum :

    01.01.2006


    Format / Umfang :

    AIAA Paper 2006-3886


    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




    Control of Separated Boundary Layer by Means of Micro- Actuated Delta Wings

    Lori, Augusto / Xantos, Savvas / Ardebili, Mahmoud et al. | AIAA | 2006


    Control of Separated Flow Using Actuated Compliant Membrane Wings

    Bohnker, Jillian R. / Breuer, Kenneth S. | AIAA | 2019


    Control of separated flows over membrane wings

    Bohnker, Jillian / Breuer, Kenny S. | AIAA | 2018


    Vortex Control on Delta Wings

    Barberis, Didier / Molton, Pascal / Renac, Florent et al. | AIAA | 2004


    Instabilities in the shear layer of delta wings

    Gordnier, Raymond / Visbal, Miguel | AIAA | 1995