Method developed for measuring wavelengths of crossflow vortices by using surface-mounted, microthin, multielement hot-film sensors. Provides direct and true value of wavelength of crossflow vortices at various spanwise locations without localized flow disturbances. Attainment of laminar airflow on aircraft wings has significant potential for reducing drag and increasing fuel efficiency.


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    Title :

    Measurement Of Crossflow Vortex Structure


    Contributors:

    Published in:

    Publication date :

    1994-10-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English





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