This part describes the results of a survey conducted to determine the present and the estimated 1970 capabilities of sensors applicable to the control of aircraft propulsion systems. The survey included electromechanical and fluid amplifier (fluidic) sensors for measurement of gas dynamic and static properties as well as for measurement of airframe dynamic parameters. (Author)


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    Title :

    Propulsion System Flow Stability Program (Dynamic). Part XVI. Survey of Sensors Applicable to the Control of Aircraft Propulsion Systems


    Contributors:

    Publication date :

    1968


    Size :

    134 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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