The combustion performance, and particularly the phenomenon of altitude operational limits, was studied by operating the annular combustor of a turbojet engine over a range of conditions of air flow, inlet pressure, inlet temperature, and fuel flow. Information was obtained on the combustion efficiencies, the effect on combustion of inlet variables, the altitude operational limits with two different fuels, the pressure losses in the combustor, the temperature and velocity profiles at the combustor outlet, the extent of afterburning, the fuel-injection characteristics, and the condition of the combustor basket.


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    Title :

    Effect of combustor-inlet conditions on performance of an annular turbojet combustor


    Contributors:

    Publication date :

    1947-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English



    Effect of combustor-inlet conditions on performance of Annular Turbojet Combustor

    Childs, J.H. / McCafferty, R.J. / Surine, C.W. | Engineering Index Backfile | 1947


    Effect of combustor-inlet conditions on performance of annular turbojet combustor

    Childs, J.H. / McCafferty, R.J. / Surine, O.W. | Engineering Index Backfile | 1947


    Effect of Combustor-Inlet Conditions on Performance of an Annular Turbojet Combustor

    J. H. Childs / R. J. McCaffferty / O. W. Surine | NTIS | 1947


    Effect of combustor-inlet conditions on performance of an annular turbojet combustor

    Childs, J. Howard / McCafferty, Richard J. / Surine, Oakley W. | TIBKAT | 1947


    Effect of combustor-inlet condition on performance of an annular turbojet combustor

    Childs, Howard J / Mccafferty, Richard J / Surine, Oakley W | NTRS | 1947