Analysis of the interrow flow field within a transonic axial compressor: Part 1- experimental investigation

Journal of Turbomachinery

Volumn 123, Issue 1, 2001, Pages 49-56

  Ottavy, X ^a   Trebinjac I ^a   Vouillarmet, A ^a  

^a ECOLE CENTRALE DE LYON   (France)

Author keywords

[No Author keywords available]

Indexed keywords

ANEMOMETERS; GLASS; LASER APPLICATIONS; ROTORS;

OPTICAL DISTORTIONS;

COMPRESSORS;

AXIAL COMPRESSOR; DESIGN; FLOW FIELD; MATHEMATICAL ANALYSIS; PERFORMANCE;

EID: 0034879743     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1328085     Document Type: Article

References (16)

1. F/A-18 E/F Aircraft engine (F414-GE-400)
2. An asymptotic analysis of mixing loss
3. The technical and economic relevance of understanding blade row Interaction Effects in Turbomachinery
4. Application of 3D-laser two focus velocimetry in turbomachine investigations
5. Design and experimental verification of the 3D velocimeters based on the L2F technique
6. Rotor blade-to-blade measurements using particle image velocimetry
7. Demonstration of PIV in a transonic compressor
8. Applications of three dimensional doppler global velocimetry to turbo machinery and wind tunnel flows
9. Effect of a mismatch between the buttons of variable stator vanes and the flow path in a highly loaded transonic compressor stage
10. Experimental and computational investigation of the NASA low speed centrifugal compressor flow field
11. Evaluation of beam refraction effects in a 3D laser doppler anemometry system for turbomachinery applications
12. A correction lens for laser doppler velocimeter measurements in a cylindrical tube
13. Treatment of L2F anemometer measurement volume distortions created by curved windows for turbomachinery application
14. Improvement in L2F anemometry technique for inter-blade investigations in high-speed turbomachinery