共 50 条
- [31] TIP LEAKAGE FLOW AND HEAT TRANSFER CHARACTERISTICS ON ROTOR CASING AND BLADE TIP IN AN AXIAL GAS TURBINE ENGINE: STEADY ANALYSIS [J]. HT2008: PROCEEDINGS OF THE ASME SUMMER HEAT TRANSFER CONFERENCE - 2008, VOL 2, 2009, : 635 - 644
- [33] A Study on Flow Instability in an Axial Compressor of Gas Turbine for Power Generation at Partial-Load Conditions [J]. International Journal of Gas Turbine, Propulsion and Power Systems, 2024, 15 (04): : 25 - 32
- [34] CALCULATION OF AXIAL DRIVE CENTRIFUGAL BREATHERS OF GAS-TURBINE ENGINE OIL SYSTEM [J]. IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA, 1979, (03): : 108 - 110
- [36] Development of a Throughflow-Based Simulation Tool for Preliminary Compressor Design Considering Blade Geometry in Gas Turbine Engine [J]. APPLIED SCIENCES-BASEL, 2021, 11 (01): : 1 - 22
- [37] Joint prediction of aircraft gas turbine engine axial flow compressor off-design performance and surge line based on the expanded method of generalized functions [J]. Russian Aeronautics, 2014, 57 (03): : 291 - 296
- [40] NUMERICAL INVESTIGATION ON AERODYNAMIC CHARACTERISTICS OF VARIABLE GEOMETRY TURBINE VANE CASCADE FOR MARINE GAS TURBINES [J]. PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, VOL 8, 2020,