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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    Titel :

    Calibration of Averaging Total Pressure Flight Wake Rake and Natural-Laminar-Flow Airfoil Drag Certification


    Beteiligte:
    E. Irani (Autor:in) / M. H. Snyder (Autor:in)

    Erscheinungsdatum :

    1988


    Format / Umfang :

    26 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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