Abstract
Experiments were conducted with a JT8D-engine sized can combustor which had all the combustion and dilution air entering through the burner front face. The primary and secondary/dilution air inlet geometries the primary fuel injection configuration, the air inlet conditions and the fuel flow rates for the combustor were varied in a series of parametric low power combustion experiments. Measurements included exit plane emissions, total pressure and total temperature distributions and burner liner temperature distributions. Attractive emission levels, temperature pattern factors and wall temperatures were achieved with low burner pressure losses for the good combinations of geometry and flow conditions.
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