Hot wire anemometer measurements have been made in the vaneless diffuser of a 1 metre diameter low speed backswept centrifugal compressor using a phase lock loop technique. Radial, tangential and axial velocity measurements have been made on eight measurement planes through the diffuser. The flow field at the diffuser entry clearly shows the impeller jet-wake flow pattern and the blade wakes. The passage wake is located on the shroud side of the diffuser and mixes out slowly as the flow moves through the diffuser. The blade wakes, on the other hand, distort and mix out rapidly in the diffuser. Contours of turbulent kinetic energy are also presented on each of the measurement stations, from which the regions of turbulent mixing can be deduced.
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ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition
May 24–27, 1993
Cincinnati, Ohio, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7888-0
PROCEEDINGS PAPER
Detailed Flow Measurements in a Centrifugal Compressor Vaneless Diffuser
Ali Pinarbasi,
Ali Pinarbasi
University of Cumhuriyet, Sivas, Turkey
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Mark W. Johnson
Mark W. Johnson
University of Liverpool, Liverpool, UK
Search for other works by this author on:
Ali Pinarbasi
University of Cumhuriyet, Sivas, Turkey
Mark W. Johnson
University of Liverpool, Liverpool, UK
Paper No:
93-GT-095, V001T03A036; 9 pages
Published Online:
February 25, 2015
Citation
Pinarbasi, A, & Johnson, MW. "Detailed Flow Measurements in a Centrifugal Compressor Vaneless Diffuser." Proceedings of the ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition. Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery. Cincinnati, Ohio, USA. May 24–27, 1993. V001T03A036. ASME. https://doi.org/10.1115/93-GT-095
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