Add to ORKGEffect of fuel distribution and flame stabilization techniques on combustion stability limits for swirl-can combustor module
Annular diffuser and combustor assembly in full scale duct burner for supersonic turbofan engin
The results of fuel-air ratio and temperature surveys made in the flame stabilizing zone of a 16-inc...
Combustion must be maintained in the turbojet-engine combustor over a wide range of operating condit...
Combustion stability limits for swirl-jet combustor modules combining air swirl and impinging jet at...
Combustion stability of single swirl-can combustor modules using ASTM-A1 liquid fue
Stability limits and efficiency of swirl can combustor modules burning natural gas fue
Emissions and performance characteristics were determined for two full annulus modular combustors op...
The blowout limits of a number of swirl-stabilized, nonpremixed flames were measured, and the observ...
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
Test results of a full annulus swirl-can combustor operated at simulated engine idle conditions indi...
Aero-engine performance is becoming an increasingly regulated aspect in aerospace indus- tries with ...
Emissions and performance characteristics were determined for full-annulus swirl-can modular combust...
Emissions and performance characteristics were determined for two full annular swirl-can combustors ...
In recent decades there has been a strong trend towards the use of lean premixed combustion in order...
Annular diffuser and combustor assembly in full scale duct burner for supersonic turbofan engin
The results of fuel-air ratio and temperature surveys made in the flame stabilizing zone of a 16-inc...
Combustion must be maintained in the turbojet-engine combustor over a wide range of operating condit...
Combustion stability limits for swirl-jet combustor modules combining air swirl and impinging jet at...
Combustion stability of single swirl-can combustor modules using ASTM-A1 liquid fue
Stability limits and efficiency of swirl can combustor modules burning natural gas fue
Emissions and performance characteristics were determined for two full annulus modular combustors op...
The blowout limits of a number of swirl-stabilized, nonpremixed flames were measured, and the observ...
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
Test results of a full annulus swirl-can combustor operated at simulated engine idle conditions indi...
Aero-engine performance is becoming an increasingly regulated aspect in aerospace indus- tries with ...
Emissions and performance characteristics were determined for full-annulus swirl-can modular combust...
Emissions and performance characteristics were determined for two full annular swirl-can combustors ...
In recent decades there has been a strong trend towards the use of lean premixed combustion in order...
Annular diffuser and combustor assembly in full scale duct burner for supersonic turbofan engin
The results of fuel-air ratio and temperature surveys made in the flame stabilizing zone of a 16-inc...
Combustion must be maintained in the turbojet-engine combustor over a wide range of operating condit...