A test program was conducted to obtain the damping characteristics of the vanes and to provide a flow calibration of a newly developed flight path accelerometer (FPA). After earlier calibration results identified an interference problem from the sideslip vane strut on the angle-of-attack vanes, the sideslip vane was moved rearward, necessitating additional calibration tests. Results are reported. (Author)


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    Titel :

    Wind Tunnel Test Results on a Flight Path Accelerometer at Subsonic and Supersonic Speeds


    Beteiligte:
    J. C. Uselton (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    20 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch