共 28 条
[1]
Foust M J, Thomsen D, Stickles R, Et al., Development of the GE Aviation Low Emission TAPS Combustor for Next Generation Aircraft Engines
[2]
Mongia H C., TAPS-A 4th Generation Propulsion Combustor Technology for Low Emissions
[3]
Hicks Y, Tedder S A, Anderson R C, Et al., NASA Numerical and Experimental Evaluation of UTRC Low Emissions Injector
[4]
Lazik W, Doerr T, Bake S, Et al., Development of Lean-Burn Low-NO<sub>x</sub> Combustion Technology at Rolls-Royce Deutschland
[5]
Yamamoto T, Shimodaira K, Kurosawa Y, Et al., Evaluation of Lean Axially Staged Combustion by Multi-Sector Combustor Tests under Low Cycle Conditions of a Small Aircraft Engine
[6]
Yamamoto T, Shimodaira K, Kurosawa Y, Et al., Research and Development of Staging Fuel Nozzle for Aeroengine
[7]
Makida M, Kurosawa Y, Yamada H., Influence of Injection Ratio of Dual-Injection Type Air-Blast Fuel Nozzle on Emission Characteristics Applied to Rectangular Single-Sector Combustor under Atmospheric Condition
[8]
1
[9]
Wang B, Zhang C, Lin Y Z, Et al., Influence of Main Swirler Vane Angle on the Ignition Performance of TELESS-II Combustor
[10]
Mi X, Zhang C, Wang B, Et al., Influence of Main Stage Air Splits on the Ignition Performance of TELESS-II Combustor