Variation, with flight conditions and engine operating variables, of thrust per sq ft of engine frontal area, specific weight, thrust specific fuel consumption, ultimate range, and range with payload, discussed.


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    Title :

    Performance and load-range characteristics of turbojet engine in transonic speed range


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1950


    Size :

    46 pages


    Remarks:

    Charts, Tables


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English