Add to ORKGThis is for an invited lecture at Cleveland State University for a combustion course. The presentation gives an overview of some of the optical diagnostic techniques the Combustion Branch uses to characterize research fuel injection concepts to reduce emissions. Examples are provided that come from previously presented conference paper
Gasoline direct injection with spray-guided charge formation is one of the most promising concepts t...
An experimental program was conducted to track the variation in soot loading in a generic gas turbin...
Research and development in the control of combustion in gas turbines. Combustion processes play ...
Researchers at the NASA Glenn Research Center, in collaboration with industry, are reducing gas turb...
A facility that allows interrogation of combusting flows by advanced diagnostic methods and instrume...
In aviation gas turbine combustors, many factors, such as the degree and extent of fuel/air mixing a...
Increasingly severe constraints on emissions, noise and fuel efficiency must be met by the next gene...
The continuing improvement of aircraft gas turbine engine operating efficiencies involves increases ...
This paper summarizes the development of lean direct injection (LDI) combustor technology at, or in ...
This paper highlights the use of two-dimensional data to characterize a multipoint swirl-venturi inj...
Lean direct injection (LDI) is a combustion concept to reduce oxides of nitrogen (NOx) for next gene...
TutorialThis tutorial provides a general overview of the state of gas turbine combustion technology....
This presentation summarizes progress to date at GE Aircraft Engines in demonstration of a lean comb...
Advanced emission reduction techniques for five existing aircraft gas turbine engines are evaluated....
The topics covered include the following: NASA High Speed Research (HSR) ozone research objectives; ...
Gasoline direct injection with spray-guided charge formation is one of the most promising concepts t...
An experimental program was conducted to track the variation in soot loading in a generic gas turbin...
Research and development in the control of combustion in gas turbines. Combustion processes play ...
Researchers at the NASA Glenn Research Center, in collaboration with industry, are reducing gas turb...
A facility that allows interrogation of combusting flows by advanced diagnostic methods and instrume...
In aviation gas turbine combustors, many factors, such as the degree and extent of fuel/air mixing a...
Increasingly severe constraints on emissions, noise and fuel efficiency must be met by the next gene...
The continuing improvement of aircraft gas turbine engine operating efficiencies involves increases ...
This paper summarizes the development of lean direct injection (LDI) combustor technology at, or in ...
This paper highlights the use of two-dimensional data to characterize a multipoint swirl-venturi inj...
Lean direct injection (LDI) is a combustion concept to reduce oxides of nitrogen (NOx) for next gene...
TutorialThis tutorial provides a general overview of the state of gas turbine combustion technology....
This presentation summarizes progress to date at GE Aircraft Engines in demonstration of a lean comb...
Advanced emission reduction techniques for five existing aircraft gas turbine engines are evaluated....
The topics covered include the following: NASA High Speed Research (HSR) ozone research objectives; ...
Gasoline direct injection with spray-guided charge formation is one of the most promising concepts t...
An experimental program was conducted to track the variation in soot loading in a generic gas turbin...
Research and development in the control of combustion in gas turbines. Combustion processes play ...