Gaseous emission from a TFE 731-2 turbofan engine were measured over a range of fuel-air ratios from idle to full power at simulated from near sea level to 13,200 m. Carbon monoxide and unburned hydrocarbon emissions were highest at idle and lowest at high power settings; oxides of nitrogen exhibited the reverse trend. Carbon monoxide and unburned hydrocarbon levels decreased with increasing altitude. Oxides of nitrogen emissions were successfully correlated by a parametric group of combustor operating variables
Projected minimum levels of engine exhaust emissions that may be practicably achievable for future c...
An annular gas turbine combustor was tested with heated natural gas fuel to determine the effect of ...
Pollutant levels of oxides of nitrogen, unburned hydrocarbons, and carbon monoxide were measured for...
Gaseous emissions from a JT8D-109 turbofan engine were measured in an altitude facility at four simu...
Emissions of total oxides of nitrogen, unburned hydrocarbons, carbon monoxide, and carbon dioxide fr...
Emissions of carbon dioxide, total oxides of nitrogen, unburned hydrocarbons, and carbon monoxide fr...
Emissions of total oxides of nitrogen, nitric oxide, unburned hydrocarbons, carbon monoxide, and car...
Emissions of total oxides of nitrogen, unburned hydrocarbons, and carbon monoxide from a J-58 engine...
Emissions of total oxides of nitrogen, unburned hydrocarbons, carbon monoxide, and carbon dioxide fr...
Gaseous fission measurements from jet engine afterburners over range of fuel-air ratio
Advanced emission reduction techniques for five existing aircraft gas turbine engines are evaluated....
A full scale double-annular ram-induction combustor designed for Mach 3.0 cruise operation was teste...
Exhaust concentrations of total unburned hydrocarbons, carbon monoxide, and nitric oxide were measur...
A program was performed to evolve and demonstrate advanced combustor technology aimed at achieving t...
Gaseous and particle emission assessments on a 1.15 kN-thrust turbojet engine were conducted at five...
Projected minimum levels of engine exhaust emissions that may be practicably achievable for future c...
An annular gas turbine combustor was tested with heated natural gas fuel to determine the effect of ...
Pollutant levels of oxides of nitrogen, unburned hydrocarbons, and carbon monoxide were measured for...
Gaseous emissions from a JT8D-109 turbofan engine were measured in an altitude facility at four simu...
Emissions of total oxides of nitrogen, unburned hydrocarbons, carbon monoxide, and carbon dioxide fr...
Emissions of carbon dioxide, total oxides of nitrogen, unburned hydrocarbons, and carbon monoxide fr...
Emissions of total oxides of nitrogen, nitric oxide, unburned hydrocarbons, carbon monoxide, and car...
Emissions of total oxides of nitrogen, unburned hydrocarbons, and carbon monoxide from a J-58 engine...
Emissions of total oxides of nitrogen, unburned hydrocarbons, carbon monoxide, and carbon dioxide fr...
Gaseous fission measurements from jet engine afterburners over range of fuel-air ratio
Advanced emission reduction techniques for five existing aircraft gas turbine engines are evaluated....
A full scale double-annular ram-induction combustor designed for Mach 3.0 cruise operation was teste...
Exhaust concentrations of total unburned hydrocarbons, carbon monoxide, and nitric oxide were measur...
A program was performed to evolve and demonstrate advanced combustor technology aimed at achieving t...
Gaseous and particle emission assessments on a 1.15 kN-thrust turbojet engine were conducted at five...
Projected minimum levels of engine exhaust emissions that may be practicably achievable for future c...
An annular gas turbine combustor was tested with heated natural gas fuel to determine the effect of ...
Pollutant levels of oxides of nitrogen, unburned hydrocarbons, and carbon monoxide were measured for...