Two 72-swirl-can-module combustors were investigated in a full annular combustor test facility at engine idle conditions typical of a 30:1 pressure-ratio engine. The effects of radial and circumferential fuel scheduling on combustion efficiency and gaseous pollutants levels were determined. Test conditions were inlet-air temperature, 452 K; inlet total pressure, 34.45 newtons per square centimeter; and reference velocity, 19.5 meters per second. A maximum combustion efficiency of 98.1 percent was achieved by radial scheduling of fuel to the inner row of swirl-can modules. Emission index values were 6.9 for unburned hydrocarbons and 50.6 for carbon monoxide at a fuel-air ratio of 0.0119. Circumferential fuel scheduling of two 90 degree secto...
Exhaust concentrations of total unburned hydrocarbons, carbon monoxide, and nitric oxide were measur...
The effect of full-annular swirling-flow on a flow-zone combustor design is investigated. Swirl flow...
A test program was undertaken to determine if variable combustor geometry could be used to reduce ex...
Test results of a full annulus swirl-can combustor operated at simulated engine idle conditions indi...
A test program was conducted to evaluate the performance and gaseous-pollutant levels of an experime...
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 ...
Exhaust pollutant emissions were measured from single swirl-can combustor modules operating over a p...
Emissions and performance characteristics were determined for full-annulus swirl-can modular combust...
Emissions and performance characteristics were determined for two full annulus modular combustors op...
Techniques were evaluated to determine if simple combustor modifications could be used to reduce the...
A full scale double-annular ram-induction combustor designed for Mach 3.0 cruise operation was teste...
A high-pressure combustor segment 0.456 meter (18 in.) long with a maximum cross section of 0.153 by...
A model which predicts nitric oxide and carbon monoxide emissions from a swirl can modular combustor...
Improved designs of swirl-can combustor modules were tested using seven-module arrays in a combustor...
Exhaust concentrations of total unburned hydrocarbons, carbon monoxide, and nitric oxide were measur...
The effect of full-annular swirling-flow on a flow-zone combustor design is investigated. Swirl flow...
A test program was undertaken to determine if variable combustor geometry could be used to reduce ex...
Test results of a full annulus swirl-can combustor operated at simulated engine idle conditions indi...
A test program was conducted to evaluate the performance and gaseous-pollutant levels of an experime...
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 ...
Exhaust pollutant emissions were measured from single swirl-can combustor modules operating over a p...
Emissions and performance characteristics were determined for full-annulus swirl-can modular combust...
Emissions and performance characteristics were determined for two full annulus modular combustors op...
Techniques were evaluated to determine if simple combustor modifications could be used to reduce the...
A full scale double-annular ram-induction combustor designed for Mach 3.0 cruise operation was teste...
A high-pressure combustor segment 0.456 meter (18 in.) long with a maximum cross section of 0.153 by...
A model which predicts nitric oxide and carbon monoxide emissions from a swirl can modular combustor...
Improved designs of swirl-can combustor modules were tested using seven-module arrays in a combustor...
Exhaust concentrations of total unburned hydrocarbons, carbon monoxide, and nitric oxide were measur...
The effect of full-annular swirling-flow on a flow-zone combustor design is investigated. Swirl flow...
A test program was undertaken to determine if variable combustor geometry could be used to reduce ex...