Test results of a full annulus swirl-can combustor operated at simulated engine idle conditions indicated that significant improvements in combustion efficiency and accompanying reductions in pollutants could be realized with radial scheduling of fuel. Test conditions were an inlet air temperature of 478 K, a pressure of 4 atmospheres, and a reference velocity of 26 meters per second. At a fuel-air ratio of 0.008, radial scheduling of fuel increased combustion efficiency from less than 50 percent with no scheduling to nearly 100 percent and produced emission index values of unburned hydrocarbons and carbon monoxide of 10 and 40, respectively
A full-scale annular turbojet combustor was tested with natural gas fuel heated from ambient tempera...
A full scale double-annular ram-induction combustor designed for Mach 3.0 cruise operation was teste...
Stability limits and efficiency of swirl can combustor modules burning natural gas fue
Two 72-swirl-can-module combustors were investigated in a full annular combustor test facility at en...
Pollutant levels of oxides of nitrogen, unburned hydrocarbons, and carbon monoxide were measured for...
Emissions and performance characteristics were determined for two full annular swirl-can combustors ...
Techniques were evaluated to determine if simple combustor modifications could be used to reduce the...
Emissions and performance characteristics were determined for full-annulus swirl-can modular combust...
A full-scale annular swirl can combustor equipped with diffuser bleed capability was tested at low f...
A test program was undertaken to determine if variable combustor geometry could be used to reduce ex...
A test program was conducted to evaluate the performance and gaseous-pollutant levels of an experime...
Emissions and performance characteristics were determined for two full annulus modular combustors op...
Exhaust pollutant emissions were measured from single swirl-can combustor modules operating over a p...
The effect of full-annular swirling-flow on a flow-zone combustor design is investigated. Swirl flow...
Evaluating performance of swirl can turbojet combustor at simulated supersonic inlet condition
A full-scale annular turbojet combustor was tested with natural gas fuel heated from ambient tempera...
A full scale double-annular ram-induction combustor designed for Mach 3.0 cruise operation was teste...
Stability limits and efficiency of swirl can combustor modules burning natural gas fue
Two 72-swirl-can-module combustors were investigated in a full annular combustor test facility at en...
Pollutant levels of oxides of nitrogen, unburned hydrocarbons, and carbon monoxide were measured for...
Emissions and performance characteristics were determined for two full annular swirl-can combustors ...
Techniques were evaluated to determine if simple combustor modifications could be used to reduce the...
Emissions and performance characteristics were determined for full-annulus swirl-can modular combust...
A full-scale annular swirl can combustor equipped with diffuser bleed capability was tested at low f...
A test program was undertaken to determine if variable combustor geometry could be used to reduce ex...
A test program was conducted to evaluate the performance and gaseous-pollutant levels of an experime...
Emissions and performance characteristics were determined for two full annulus modular combustors op...
Exhaust pollutant emissions were measured from single swirl-can combustor modules operating over a p...
The effect of full-annular swirling-flow on a flow-zone combustor design is investigated. Swirl flow...
Evaluating performance of swirl can turbojet combustor at simulated supersonic inlet condition
A full-scale annular turbojet combustor was tested with natural gas fuel heated from ambient tempera...
A full scale double-annular ram-induction combustor designed for Mach 3.0 cruise operation was teste...
Stability limits and efficiency of swirl can combustor modules burning natural gas fue