Pollutant formation in fuel lean reciruclating flows, Volume 2785
Robert W. Schefer, Robert F. Sawyer, United States. National Aeronautics and Space Administration, University of California, Berkeley
National Aeronautics and Space Administration, 1976 - Aircraft exhaust emissions - 219 pages
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aircraft approximately Axial concentration C^Hg chemiluminescent cold flow Combustion Institute combustion process combustion zone combustor centerline combustor exit concentration and temperature conservation equations constant dependent variable Engineering equivalence ratio Experimental and predicted flame temperature flame zone flamefront flowfield fuel and air fuel lean gas turbine gas turbine combustors high temperature hydrocarbon inlet conditions jet exit jet injector jet stream kinetic location of 1.4 main stream inlet mass fraction maximum mechanism meter mole fraction mole fraction distributions N0X emissions Nitric Oxide OICO OIOO opposed reacting jet OTOO oxides of nitrogen partial equilibrium Predicted and experimental premixed present investigation pressure PRINT propane propane oxidation quenching RADIAL DISTANCE radial location reaction recirculation zone residence shown in Figure stability limits stream equivalence ratio stream function SUBROUTINE temperature distributions temperature profiles temperature regions test section thermocouple tion turbulent upstream viscosity vorticity Vycor