Survey of general requirements for performance and control of supersonic inlets for turbojet or turbofan propulsion systems for supersonic transport; interaction between inlet and engine performance are considered and effects of pressure recovery, bleed flows, and external drags on engine thrust and specific fuel consumption for design and off-design operation; problem of controlling inlet to obtain safe and efficient operation; effects of control tolerances on inlet geometry and terminal shock position on engine performance are also shown; possible approaches for simplifying or improving inlet control system.


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    Title :

    Engine air inlet compatibility for supersonic transport


    Additional title:

    SAE -- Paper


    Contributors:
    Kepler, C.E. (author) / Barry, F.W. (author)

    Conference:

    SAE Meeting ; 1965 Inlets



    Publication date :

    1965


    Size :

    34 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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