A test program was conducted to evaluate the performance and gaseous-pollutant levels of an experimental full-annulus 72-module swirl-can combustor. A comparison of data with those for a 120-module swirl-can combustor showed no significant difference in performance or levels of gaseous pollutants. Oxides of nitrogen were correlated for the 72- and 120-swirl-can combustors by using a previously developed parameter
The effect of full-annular swirling-flow on a flow-zone combustor design is investigated. Swirl flow...
Full annular versions of advanced combustor designs, sized to fit within the CF6-50 engine, were def...
The generation of technology was studied for the development of advanced commercial CTOL aircraft en...
Exhaust pollutant emissions were measured from single swirl-can combustor modules operating over a p...
Two 72-swirl-can-module combustors were investigated in a full annular combustor test facility at en...
Emissions and performance characteristics were determined for full-annulus swirl-can modular combust...
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 ...
Improved designs of swirl-can combustor modules were tested using seven-module arrays in a combustor...
Test results of a full annulus swirl-can combustor operated at simulated engine idle conditions indi...
Emissions and performance characteristics were determined for two full annulus modular combustors op...
A full scale double-annular ram-induction combustor designed for Mach 3.0 cruise operation was teste...
A model which predicts nitric oxide and carbon monoxide emissions from a swirl can modular combustor...
Exhaust concentrations of total unburned hydrocarbons, carbon monoxide, and nitric oxide were measur...
A program was performed to evolve and demonstrate advanced combustor technology aimed at achieving t...
The effect of full-annular swirling-flow on a flow-zone combustor design is investigated. Swirl flow...
Full annular versions of advanced combustor designs, sized to fit within the CF6-50 engine, were def...
The generation of technology was studied for the development of advanced commercial CTOL aircraft en...
Exhaust pollutant emissions were measured from single swirl-can combustor modules operating over a p...
Two 72-swirl-can-module combustors were investigated in a full annular combustor test facility at en...
Emissions and performance characteristics were determined for full-annulus swirl-can modular combust...
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 ...
Improved designs of swirl-can combustor modules were tested using seven-module arrays in a combustor...
Test results of a full annulus swirl-can combustor operated at simulated engine idle conditions indi...
Emissions and performance characteristics were determined for two full annulus modular combustors op...
A full scale double-annular ram-induction combustor designed for Mach 3.0 cruise operation was teste...
A model which predicts nitric oxide and carbon monoxide emissions from a swirl can modular combustor...
Exhaust concentrations of total unburned hydrocarbons, carbon monoxide, and nitric oxide were measur...
A program was performed to evolve and demonstrate advanced combustor technology aimed at achieving t...
The effect of full-annular swirling-flow on a flow-zone combustor design is investigated. Swirl flow...
Full annular versions of advanced combustor designs, sized to fit within the CF6-50 engine, were def...
The generation of technology was studied for the development of advanced commercial CTOL aircraft en...