The topics covered include the following: NASA High Speed Research (HSR) ozone research objectives; NO(x) formation; emission reduction; High Speed Civil Transport (HSCT) supersonic cruise combustion operating conditions; NO(x) correlations; typical NO(x) characteristics of a current technology and low NO(x) combustors; HSCT emission reduction strategies; variation of NO(x) with equivalence ratio; the Emission Reduction Program; and emission reduction milestones
Combustor test rig results indicate that substantial reductions from current emission levels of carb...
This paper presents the nitrogen oxides, carbon monoxide, and particulate matter emissions of a sing...
Two P&W (Pratt & Whitney)'s axially staged sector combustors have been developed under NASA's Enviro...
Advanced emission reduction techniques for five existing aircraft gas turbine engines are evaluated....
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...
Increasing the pressure and temperature of the engines of a new generation of supersonic airliners i...
Increasing the pressure and temperature of the engines of new generation supersonic airliners increa...
In accordance with NASAs technology goals for future subsonic vehicles, this contract identified and...
The chance for future long range high speed commercial transport leads to a more comprehensive inves...
An array of experiments designed to explore the potential of advanced combustion techniques for cont...
The feasibility of employing the known attractive and distinguishing features of catalytic combustio...
The Advanced Low Emissions Catalytic Combustors Program (ALECC) is being undertaken to evaluate the ...
An overview of research efforts at NASA Glenn Research Center (GRC) in low-emission combustion techn...
Gas turbine engine combustor technology for the reduction of pollutant emissions is summarized. Vari...
Combustor test rig results indicate that substantial reductions from current emission levels of carb...
This paper presents the nitrogen oxides, carbon monoxide, and particulate matter emissions of a sing...
Two P&W (Pratt & Whitney)'s axially staged sector combustors have been developed under NASA's Enviro...
Advanced emission reduction techniques for five existing aircraft gas turbine engines are evaluated....
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...
Increasing the pressure and temperature of the engines of a new generation of supersonic airliners i...
Increasing the pressure and temperature of the engines of new generation supersonic airliners increa...
In accordance with NASAs technology goals for future subsonic vehicles, this contract identified and...
The chance for future long range high speed commercial transport leads to a more comprehensive inves...
An array of experiments designed to explore the potential of advanced combustion techniques for cont...
The feasibility of employing the known attractive and distinguishing features of catalytic combustio...
The Advanced Low Emissions Catalytic Combustors Program (ALECC) is being undertaken to evaluate the ...
An overview of research efforts at NASA Glenn Research Center (GRC) in low-emission combustion techn...
Gas turbine engine combustor technology for the reduction of pollutant emissions is summarized. Vari...
Combustor test rig results indicate that substantial reductions from current emission levels of carb...
This paper presents the nitrogen oxides, carbon monoxide, and particulate matter emissions of a sing...
Two P&W (Pratt & Whitney)'s axially staged sector combustors have been developed under NASA's Enviro...
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