Separate development of intake and nozzle may lead to components which are individually very efficient; when integrated into unit some of efficiency may be lost in producing compatibility with engine and remainder of powerplant; it is often found that the most efficient components lack flexibility in face of changing atmospheric conditions; flexibility can be achieved by suitable development and choice of components which would reduce demands on intake control system without incurring severe penalty in performance; problem is treated in terms of quasi-static effects of changes in ambient temperature on performance.


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    Title :

    Fully integrated propulsion system for supersonic transport aircraft


    Additional title:

    AGARDograph


    Contributors:
    Talbot, J.E. (author) / Furness, B. (author)


    Publication date :

    1965


    Size :

    26 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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