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.
Exhaust emissions of a double annular combustor: Parametric study
1974-02-01
Report
No indication
English
Particulate exhaust emissions from an experimental combustor
TIBKAT | 1975
|Single Annular comBustor for Emissions Reduction: Technology Development for Small Engines
British Library Conference Proceedings | 2011
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