共 50 条
- [21] BENEFITS OF ACTIVE COMPRESSOR STABILITY MANAGEMENT ON TURBOFAN ENGINE OPERABILITY [J]. PROCEEDINGS OF THE ASME TURBO EXPO 2008, VOL 2, 2008, : 303 - 314
- [22] Power extraction method for acceleration and deceleration control law design of turbofan engine [J]. Hangkong Dongli Xuebao/Journal of Aerospace Power, 2009, 24 (04): : 867 - 874
- [23] Fixed states method of turbofan engine acceleration and deceleration control law design [J]. Hangkong Dongli Xuebao/Journal of Aerospace Power, 2022, 37 (12): : 2896 - 2904
- [24] Benefits of Active Compressor Stability Management on Turbofan Engine Operability [J]. JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2009, 131 (04):
- [25] Research and experiment on improved sectional combination control scheme for civil turbofan engine's startup process [J]. 1600, Beijing University of Aeronautics and Astronautics (BUAA) (29):
- [26] Aerodynamic computation of a scramjet engine on vector-parallel supercomputers [J]. PARALLEL COMPUTATIONAL FLUID DYNAMICS: NEW FRONTIERS AND MULTI-DISCIPLINARY APPLICATIONS, PROCEEDINGS, 2003, : 173 - 180
- [27] Effects of Heating of Turbine on Turbofan Engine Compressor Tip Clearance During Acceleration Process [J]. Tuijin Jishu/Journal of Propulsion Technology, 2020, 41 (05): : 1144 - 1151