An array of experiments designed to explore the potential of advanced combustion techniques for controlling the emissions of aircraft into the upper atmosphere was discussed. Of particular concern are the oxides of nitrogen (NOx) emissions into the stratosphere. The experiments utilize a wide variety of approaches varying from advanced combustor concepts to fundamental flame tube experiments. Results are presented which indicate that substantial reductions in cruise NOx emissions should be achievable in future aircraft engines. A major NASA program is described which focuses the many fundamental experiments into a planned evolution and demonstration of the prevaporized-premixed combustion technique in a full-scale engine
Combustor research programs are described whose purpose is to demonstrate significantly lower exhaus...
Emissions of carbon dioxide, total oxides of nitrogen, unburned hydrocarbons, and carbon monoxide fr...
In accordance with NASAs technology goals for future subsonic vehicles, this contract identified and...
Advanced emission reduction techniques for five existing aircraft gas turbine engines are evaluated....
Gas turbine engine combustor technology for the reduction of pollutant emissions is summarized. Vari...
The application of lean, premixed, prevaporized combustion to aircraft turbine engine systems can re...
Effective emission control techniques have been identified and a wide spectrum of potential applicat...
The topics covered include the following: NASA High Speed Research (HSR) ozone research objectives; ...
To accomplish simultaneous reduction of unburned hydrocarbons, carbon monoxide, and oxides of nitrog...
An overview of the ongoing program is presented. Objectives, plan, schedule, pollution and performan...
Analytical studies have been conducted to determine the best methods of reducing NO(x) emissions fro...
Emissions of total oxides of nitrogen, unburned hydrocarbons, carbon monoxide, and carbon dioxide fr...
Combustor test rig results indicate that substantial reductions from current emission levels of carb...
Increasing the pressure and temperature of the engines of new generation supersonic airliners increa...
An overview of research efforts at NASA Glenn Research Center (GRC) in low-emission combustion techn...
Combustor research programs are described whose purpose is to demonstrate significantly lower exhaus...
Emissions of carbon dioxide, total oxides of nitrogen, unburned hydrocarbons, and carbon monoxide fr...
In accordance with NASAs technology goals for future subsonic vehicles, this contract identified and...
Advanced emission reduction techniques for five existing aircraft gas turbine engines are evaluated....
Gas turbine engine combustor technology for the reduction of pollutant emissions is summarized. Vari...
The application of lean, premixed, prevaporized combustion to aircraft turbine engine systems can re...
Effective emission control techniques have been identified and a wide spectrum of potential applicat...
The topics covered include the following: NASA High Speed Research (HSR) ozone research objectives; ...
To accomplish simultaneous reduction of unburned hydrocarbons, carbon monoxide, and oxides of nitrog...
An overview of the ongoing program is presented. Objectives, plan, schedule, pollution and performan...
Analytical studies have been conducted to determine the best methods of reducing NO(x) emissions fro...
Emissions of total oxides of nitrogen, unburned hydrocarbons, carbon monoxide, and carbon dioxide fr...
Combustor test rig results indicate that substantial reductions from current emission levels of carb...
Increasing the pressure and temperature of the engines of new generation supersonic airliners increa...
An overview of research efforts at NASA Glenn Research Center (GRC) in low-emission combustion techn...
Combustor research programs are described whose purpose is to demonstrate significantly lower exhaus...
Emissions of carbon dioxide, total oxides of nitrogen, unburned hydrocarbons, and carbon monoxide fr...
In accordance with NASAs technology goals for future subsonic vehicles, this contract identified and...