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Keyword [Tip-leakage vortex]
Result: 1 - 20 | Page: 1 of 2
1. The Interactive Unsteady Mechanism Between Tip Leakage Vortex, Stall Inception And Micro Tip Injection In Low-Speed Axial Compressor
2. Numerical Simulation Of Using Blade Tip Winglet In Plane Compressor Cascade
3. Experimental And Numerical Research On Flow Characteristic Of Low Pressure Axial Fan With Circumferential Skew Rotor Blades
4. Stability Enhancement Technology Of Tip Air Injection In Axial Flow Compressor-Mechanism And Intelligent Control
5. Investigation Of The Mechanisms For Stall Margin Improvement And Design Methods Of Casing Treatments In Transonic Compressors
6. Numerical And Physical Investigation Of Tip Leakage Vortex Cavitating Flows
7. Research On Tip Leakage Vortex Structure And Cavitation Mechanism In Three-Dimensional Hydrofoil And Axial Flow Pump
8. Study On The Characteristics Of The Blade Tip Leakage Vortex Flow And The Cavitating Flow Field
9. A Study On The Endwall Unsteady Flow And Loss Of Highly-Loaded Turbine
10. Numerical Simulation And Experiments Of The Flow Instability In Mixed-Flow Pump
11. The Numerical Investigation Of Blade Tip's Stall In A Transonic Compressor Rotor
12. Aerodynamic Mechanism Analysis And Experimental Research Of A Counter-rotating Compressor With Boundary Layer Suction
13. Investigation On The Influence Mechanism Of Wake Vortex Migrating On The Tip Clearance Flow In A Counter-rotating Compressor
14. Research On The Tip Vortex Structure And Unsteady Flow Control Of Compressor Cascade
15. Study On The Effect Of The Aerodynamic Performance Of Axial Fan With Tip End-plate
16. Study On The Influence Of Tip Clearance Leakage Flow On Stall Characteristics Of Semi-open Centrifugal Pump
17. Numerical Study On The Influence Of Tip Clearance On Turbine Performance
18. Numerical Study On The Influence Of Tip Winglet On The Performance Of Transonic Fan Rotor
19. Numerical Study On The Influence Of Tip Winglet On The Performance Of Centrifugal Compressor
20. Discussion On Evolution Mechanism Of The Tip Leakage Vortex With Unsteady Plasma Actuation
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