A two-color, five-beam LDV system has been configured to make simultaneous three-component velocity measurements of the flow field in a two-stage axial compressor model. The system has been used to make time-resolved measurements both between compressor blade rows as well as within the rotating blade passages in an axial compressor. The data show the nature and behavior of the complex, three-dimensional flow phenomena present in the tip region of a compressor as they convect downstream. In particular, the nature of the tip leakage vortex is apparent, being manifested by high blockage as well as the expected vortical motion. The data indicate that the radial flows associated with the tip leakage vortex begin to decrease while within the rotor passage, and that they temporarily increase aft of the passage.
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ASME 1992 International Gas Turbine and Aeroengine Congress and Exposition
June 1–4, 1992
Cologne, Germany
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7893-4
PROCEEDINGS PAPER
Measurement of the Three-Dimensional Tip Region Flowfield in an Axial Compressor
R. C. Stauter
R. C. Stauter
United Technologies Research Center, East Hartford, CT
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R. C. Stauter
United Technologies Research Center, East Hartford, CT
Paper No:
92-GT-211, V001T01A072; 10 pages
Published Online:
March 3, 2015
Citation
Stauter, RC. "Measurement of the Three-Dimensional Tip Region Flowfield in an Axial Compressor." Proceedings of the ASME 1992 International Gas Turbine and Aeroengine Congress and Exposition. Volume 1: Turbomachinery. Cologne, Germany. June 1–4, 1992. V001T01A072. ASME. https://doi.org/10.1115/92-GT-211
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