Description of a three-year exploratory research program for the design, development, and flight evaluation of an Integrated Propulsion Control System (IPCS). The primary objectives of this program are to establish through flight test the potential improvements in steady-state and transient propulsion system performance that can be achieved as a direct result of new modes of control, more direct sensing of engine and inlet parameters, and the use of more sophisticated, high-speed digital computation. A F-111 E aircraft with the left inlet and engine modified to the IPCS configuration will be used to conduct the flight evaluation.


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    Title :

    Integrated Propulsion Control System program.


    Contributors:

    Conference:

    Air Transportation Meeting ; 1973 ; Miami, FL


    Publication date :

    1973-04-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Integrated Propulsion Control System Program

    Bentz, Charles E. / Zeller, John R. | SAE Technical Papers | 1973


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