Paper

achieved addition analysis applications ASME axial burner calculated cell combustion combustor compared components compressor computed concentration configuration cooling cost cycle decrease developed distribution effect efficiency engine equivalence ratio exhaust exit experimental experiments Figure flame flow flow rate formation formed fraction fuel gas turbine heat higher holes increase indicate injection injector inlet inlet temperature lean levels limit liner load loss lower mass maximum mean measured mechanism method mixing mixture natural gas Nitrogen NOx emissions nozzle obtained operating outlet overall oxidation parameters performance pilot plant predicted premixed presented pressure primary zone production radial range reaction reduced region secondary shown shows simulation specific speed stage steam swirl swirler Table temperature thermal tube turbulent values velocity wall zone