In operation of combustors for fuel evaluation at NACA Cleveland laboratory, it was found that fuel nozzle carbon deposition affects combustion efficiency and fuel nozzle shield, which prevented carbon deposition, improved reproducibility of combustion data.


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    Title :

    Effects of fuel-nozzle carbon deposition on combustion efficiency of single tubular-type, reverse-flow turbojet combustor at simulated altitude conditions


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1948


    Size :

    27 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English