The wake imaging system (WIS) for rapid mappings of wind tunnel model flowfields is described and a summary of recent results is presented. Three different types of systems are discussed. These are: In addition, progress toward developing a low intrusive WIS for high-pressure transonic wind tunnels and for flight test applications is described.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Wake Imaging System Applications at the Boeing Aerodynamics Laboratory


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    Aerospace Technology Conference and Exposition ; 1985



    Erscheinungsdatum :

    01.10.1985




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Application of Uncertainty Methodology at the Boeing Aerodynamics Laboratory

    Belter, D. L. / AIAA | British Library Conference Proceedings | 1996



    Application of Uncertainty Methodology at the Boeing Aerodynamics Laboratory

    Belter, D. L. / AIAA | British Library Conference Proceedings | 1996


    Aerodynamics of wake vortices.

    BROWN, C. E. | AIAA | 1973


    Wind turbine wake aerodynamics

    Vermeer, L.J. | Online Contents | 2003