A standard service airspeed system on a single engine research support airplane was calibrated by the trailing anenometer method. The effects of flaps, power, sideslip, and lag were evaluated. The factory supplied airspeed calibrations were not sufficiently accurate for high accuracy flight research applications. The trailing anemometer airspeed calibration was conducted to provide the capability to use the research support airplane to perform pace aircraft airspeed calibrations.


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    Title :

    Low-Speed Airspeed Calibration Data for a Single-Engine Research-Support Aircraft


    Contributors:

    Publication date :

    1980


    Size :

    22 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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