An averaging total pressure wake rake used by the Cessna Aircraft Company in flight tests of a modified 210 airplane with a laminar flow wing was calibrated in wind tunnel tests against a five-tube pressure probe. The model generating the wake was a full-scale model of the Cessna airplane wing. Indications of drag trends were the same for both instruments.


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    Title :

    Calibration of averaging total pressure flight wake rake and natural-laminar-flow airfoil drag certification


    Contributors:
    Irani, E. (author) / Snyder, M. H. (author)

    Publication date :

    1988-02-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :



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