Add to ORKGFlow measurements were performed on each of six swirl-can combustor module designs under simulated c...
A 19XB-1 combustor was operated under conditions simulating zero-ram operation of the 19XB-1 turboje...
Emissions and performance characteristics were determined for two full annulus modular combustors op...
Effect of fuel distribution and flame stabilization techniques on combustion stability limits for sw...
Combustion stability limits for swirl-jet combustor modules combining air swirl and impinging jet at...
Stability limits and efficiency of swirl can combustor modules burning natural gas fue
Combustion stability of single swirl-can combustor modules using ASTM-A1 liquid fuel.Prepared at Lew...
Evaluating performance of swirl can turbojet combustor at simulated supersonic inlet condition
A 27-inch (68.6-cm) long rectangular combustor segment consisting of an array of 48 combustor module...
Emissions and performance characteristics were determined for full-annulus swirl-can modular combust...
Performance tests of rectangular sector of turbojet combustor consisting of array of modul
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 annular swirl-can combustors ...
Combustion efficiency and performance of swirl can modules under conditions simulating operation of ...
Two 72-swirl-can-module combustors were investigated in a full annular combustor test facility at en...
Flow measurements were performed on each of six swirl-can combustor module designs under simulated c...
A 19XB-1 combustor was operated under conditions simulating zero-ram operation of the 19XB-1 turboje...
Emissions and performance characteristics were determined for two full annulus modular combustors op...
Effect of fuel distribution and flame stabilization techniques on combustion stability limits for sw...
Combustion stability limits for swirl-jet combustor modules combining air swirl and impinging jet at...
Stability limits and efficiency of swirl can combustor modules burning natural gas fue
Combustion stability of single swirl-can combustor modules using ASTM-A1 liquid fuel.Prepared at Lew...
Evaluating performance of swirl can turbojet combustor at simulated supersonic inlet condition
A 27-inch (68.6-cm) long rectangular combustor segment consisting of an array of 48 combustor module...
Emissions and performance characteristics were determined for full-annulus swirl-can modular combust...
Performance tests of rectangular sector of turbojet combustor consisting of array of modul
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 annular swirl-can combustors ...
Combustion efficiency and performance of swirl can modules under conditions simulating operation of ...
Two 72-swirl-can-module combustors were investigated in a full annular combustor test facility at en...
Flow measurements were performed on each of six swirl-can combustor module designs under simulated c...
A 19XB-1 combustor was operated under conditions simulating zero-ram operation of the 19XB-1 turboje...
Emissions and performance characteristics were determined for two full annulus modular combustors op...