共 31 条
- [24] Impact of pressure variations at inlet and outlet boundaries on aerodynamic performance of multi-stage axial compressor Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2024, 45 (19):
- [26] Numerical investigation of effect of inlet swirl and total-pressure distortion on performance and stability of an axial transonic compressor Journal of Thermal Science, 2016, 25 : 501 - 510
- [28] Numerical Investigation of Flow Structure and Pressure Drop Prediction for Radial Inflow Between Corotating Disks With Negative Effective Inlet Swirl Ratio JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2025, 147 (03):
- [29] NUMERICAL INVESTIGATION OF FLOW STRUCTURE AND PRESSURE DROP PREDICTION FOR RADIAL INFLOW BETWEEN CO-ROTATING DISCS WITH NEGATIVE EFFECTIVE INLET SWIRL RATIO PROCEEDINGS OF ASME TURBO EXPO 2024: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2024, VOL 8, 2024,
- [30] Numerical And Experimental Investigation of Aerodynamics On Flow Around A Highly Loaded Low-Pressure Turbine Blade with Flow Separation Under Steady And Periodic Unsteady Inlet Flow Condition PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2016, VOL 5A, 2016,