Compressor stability enhancement using discrete tip injection

Journal of Turbomachinery

Volumn 123, Issue 1, 2001, Pages 14-23

  Suder, K L ^a   Hathaway, M D ^a   Thorp, S A ^a   Strazisar, A J ^a   Bright, M B ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; ROTORS;

DISCRETE TIP INJECTIONS;

COMPRESSORS;

COMPRESSOR; COMPUTATIONAL FLUID DYNAMICS; MEASUREMENT METHOD; STABILITY;

EID: 0034878791     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1330272     Document Type: Article

References (31)

1. Stall margin improvement by casing treatment-its mechanism and effectiveness
2. Numerical simulation of compressor endwall and casing treatment flow phenomena
3. Active control of rotating stall in a low speed axial compressor rotor
4. Active stabilization of axial compressors with circumferential inlet distortion
5. Integrated control of rotating stall and surge in high-speed multistage compression systems
6. Characterizing the effects of air injection on compressor performance for use in active control of rotating stall
7. Active stabilization of rotating stall and surge in a transonic single stage axial compressor
8. Rotating stall control in a high-speed stage with inlet distortion: Part I-radial distortion
9. Rotating stall control in a high-speed stage with inlet distortion: Part II-circumferential distortion
10. Experiments in active control of stall on an aeroengine gas turbine
11. A study of spike and modal stall phenomena in a low-speed axial compressor
12. Effects of endwall suction and blowing on compressor stability enhancement
13. Experimental techniques for actuation, sensing, and measurement of rotating stall dynamics in high speed engines
14. Model equation for simulating flows in multistage turbomachinery
15. Impact of discrete tip injection on stabilization of a transonic compressor rotor
16. Loss sources and magnitudes in axial flow compressors
17. Stalling pressure rise capability of axial flow compressor stages
18. The role of tip clearance in high speed fan stall
19. Blockage development in a transonic, axial compressor rotor
20. Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor
21. Stall inception in axial flow compressors
22. Effects of non-axisymmetric tip clearance on axial compressor performance and stability
23. Part-circumference casing treatment and the effect on compressor stall
24. Inlet distortion generated forced response of a low-aspect-ratio transonic fan
25. Recessed casing treatment effects on fan performance and flow field
26. Rotor casing treatment