Improved hot-film anemometer developed for making high-bandwidth turbulence measurements in moderate-enthalpy supersonic and hypersonic flows (e.g., NASP inlets and control surfaces, HSCT jet exhaust). Features include low thermal inertia, ruggedness, and reduced perturbation of flow.


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    Title :

    Microsensor Hot-Film Anemometer


    Contributors:

    Published in:

    Publication date :

    1995-04-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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