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.


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    Title :

    Wake Imaging System Applications at the Boeing Aerodynamics Laboratory


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    Aerospace Technology Conference and Exposition ; 1985



    Publication date :

    1985-10-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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