A full scale double-annular ram-induction combustor designed for Mach 3.0 cruise operation was tested. Emissions of oxides of nitrogen, carbon monoxide, unburned hydrocarbons, and smoke were measured over a range of combustor operating variables including reference velocity, inlet air temperature and pressure, and exit average temperature. ASTM Jet-A fuel was used for these tests. An equation is provided relating oxides of nitrogen emissions as a function of the combustor, operating variables. A small effect of radial fuel staging on reducing exhaust emissions (which were originally quite low) is demonstrated.


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    Titel :

    Exhaust emissions of a double annular combustor: Parametric study


    Beteiligte:
    Schultz, D. F. (Autor:in)

    Erscheinungsdatum :

    01.02.1974


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch