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640 sea level 731-2 turbofan engine altitude chamber altitude test analyzer carbon dioxide Carbon Monoxide Emissions combus combustor inlet total combustor inlet-air temperature computed constant engine inlet corrected for water data taken decreased with increasing denote altitude simulation emis emission index value emissions were highest engine inlet temperature engine inlet-air temperature engine were measured exhaust gas flight Mach numbers function of combustor Gas Turbine gine high power settings highest at idle idle to full increasing altitude resulted increasing throttle index as function inlet total temperature instrument level to 13 Lewis Research Center monoxide and unburned nitrogen Carbon monoxide normalized to standard oxides of nitrogen Performing Organization Pollutant Emissions ppm g/kg fuel range of fuel-air ratios from idle report Ref sample validity sea-level pressure shown in figure SIMULATED ALTITUDE CONDITIONS simulation by pressure Solid symbols denote symbols denote altitude temperature of 294 TFE 731-2 turbofan Turbine Engines unburned hydrocarbon emissions various altitudes