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)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Contributors:

    Publication date :

    1972


    Size :

    20 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English