Infrared thermography is a preferred method investigating transition in flight: a) Global and non-intrusive; b) Can also be used to visualize and characterize other fluid mechanic phenomena such as shock impingement, separation etc. F-15 based system was updated with new camera and digital video recorder to support high Reynolds number transition tests. Digital Recording improves image quality and analysis capability and allows for accurate quantitative (temperature) measurements and greater enhancement through image processing allows analysis of smaller scale phenomena.


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    Title :

    Advanced IR System For Supersonic Boundary Layer Transition Flight Experiment


    Contributors:

    Conference:

    Fundamental Aeronautics Program Annual Meeting 2008 ; 2008 ; Atlanta, GA, United States


    Publication date :

    2008-10-07


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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