An improved design of air-atomizing fuel nozzles was determined from a study of four differently shaped splash-cone fuel nozzles after 56 hr of durability testing in a combustor segment. Test conditions included fuel-air ratios of 0.008 to 0.018, inlet-air total pressures of 41 to 203 N/cm, inlet-air temperatures of 477 to 811 K, and a reference velocity of 21.3 m/sec. Flat-tip fuel nozzles showed the least erosion damage and at a combustor operating condition of 700 K and 101 N/sq cm an oxides-of-nitrogen emission index of 12 and a smoke number of approximately 18 with a fuel-air ratio of 0.018. Emission indices for carbon monoxide and unburned hydrocarbons were 44 and 16, respectively, at simulated idle conditions of 477 K and 41 N/sq cm
Test results of a full annulus swirl-can combustor operated at simulated engine idle conditions indi...
The penetration and cone-angle of fuel sprays from open nozzles were recorded with the NACA Spray Ph...
Emissions and performance characteristics were determined for two full annulus modular combustors op...
A high-pressure combustor segment 0.456 meter (18 in.) long with a maximum cross section of 0.153 by...
Cold flow atomization tests of several different designs of swirl can combustor modules were conduct...
Tests of various fuel nozzles were conducted with natural gas fuel in a full-annulus combustor. The ...
Experimental tests with diesel number 2 and Jet A fuels were conducted in a combustor segment to obt...
Emissions and performance characteristics were determined for two full annular swirl-can combustors ...
A full-scale annular turbojet combustor was tested with natural gas fuel heated from ambient tempera...
Problems concerned with the supercritical injection concept are discussed. Supercritical injection i...
Pollutant levels of oxides of nitrogen, unburned hydrocarbons, and carbon monoxide were measured for...
The development of higher thermal stability fuels and the development of onboard fuel deoxygenation ...
Two 72-swirl-can-module combustors were investigated in a full annular combustor test facility at en...
A baseline CF6-50 combustor and three advanced combustor designs were evaluated to determine the eff...
Spray nozzles and atomizers have several applications in many forms of industry such as aerospace, a...
Test results of a full annulus swirl-can combustor operated at simulated engine idle conditions indi...
The penetration and cone-angle of fuel sprays from open nozzles were recorded with the NACA Spray Ph...
Emissions and performance characteristics were determined for two full annulus modular combustors op...
A high-pressure combustor segment 0.456 meter (18 in.) long with a maximum cross section of 0.153 by...
Cold flow atomization tests of several different designs of swirl can combustor modules were conduct...
Tests of various fuel nozzles were conducted with natural gas fuel in a full-annulus combustor. The ...
Experimental tests with diesel number 2 and Jet A fuels were conducted in a combustor segment to obt...
Emissions and performance characteristics were determined for two full annular swirl-can combustors ...
A full-scale annular turbojet combustor was tested with natural gas fuel heated from ambient tempera...
Problems concerned with the supercritical injection concept are discussed. Supercritical injection i...
Pollutant levels of oxides of nitrogen, unburned hydrocarbons, and carbon monoxide were measured for...
The development of higher thermal stability fuels and the development of onboard fuel deoxygenation ...
Two 72-swirl-can-module combustors were investigated in a full annular combustor test facility at en...
A baseline CF6-50 combustor and three advanced combustor designs were evaluated to determine the eff...
Spray nozzles and atomizers have several applications in many forms of industry such as aerospace, a...
Test results of a full annulus swirl-can combustor operated at simulated engine idle conditions indi...
The penetration and cone-angle of fuel sprays from open nozzles were recorded with the NACA Spray Ph...
Emissions and performance characteristics were determined for two full annulus modular combustors op...