Wake recovery performance benefit in a high-speed axial compressor

Journal of Turbomachinery

Volumn 124, Issue 2, 2002, Pages 275-284

  Van Zante, Dale E ^a   Adamczyk, John J ^a   Strazisar, Anthony J ^a   Okiishi, Theodore H ^a  

^a IOWA STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANEMOMETERS; AXIAL FLOW; COMPRESSORS; VELOCITY;

AXIAL COMPRESSORS;

WAKES;

AXIAL COMPRESSOR; DESIGN; LOSS; WAKE;

EID: 0036541571     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1445793     Document Type: Article

References (24)

1. Intra-stator transport of rotor wakes and its effect on compressor performance
2. Multistage compressor stator/rotor interaction
3. Wake dispersion in turbomachines
4. Wake ingestion propulsion benefit
5. Casing boundary layers in multistage axial-flow compressors
6. Wake mixing in axial flow compressors
7. Impact of rotor wakes on steady-state axial compressor performance
8. Flow measurements using a laser-two-focus anemometer in a high-speed centrifugal and a multistage axial compressor
9. Temporally and spatially resolved flow in a two-stage axial compressor: Part 1 - Experiment
10. Flow measurements in the stator row of a single-stage transonic axial-flow compressor with controlled diffusion stator blades
11. Inter and intrablade row laser velocimetry studies of gas turbine compressor flows
12. Unsteady flows in a single-stage transonic axial flow fan stator row
13. Turbulent wakes in pressure gradients
14. A transport model for the deterministic stresses associated with turbomachinery blade row interactions
15. Curvature and pressure-gradient effects on a small defect wake
16. Design and overall performance of four highly loaded, high-speed inlet stages for an advanced high-pressure-ratio core compressor
17. Model equation for simulating flows in multistage turbomachinery
18. Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.19 and 1.26. Respectively, and with design pressure ratio of 1.82
19. Laser anemometer measurements in a transonic axial-flow fan rotor
20. A new procedure for simulating unsteady flows through turbomachinery blade passages