The flow within an axial-flow spiral inducer impeller is complex and three-dimensional. The long but tightly-spiralled passages give rise to secondary flow fields strongly influenced by the blade walls. Flow analysis in such an impeller is carried out by a three-dimensional viscous flow code and compared with previously published LDV measurements. Due to the extreme blade angles of the inducer, an unconventional meshing strategy is required in order to prevent high mesh non-orthogonality. Details of that strategy are provided. Tip clearance modelling was not incorporated in this first stage of investigation. Despite this, the flow analysis reveals the pattern of development of the secondary flow field along the length of the high solidity passage consistent with the LDV data but in much greater detail than was possible with the limited capability of the measurement system. Predicted flow patterns upstream suggest preconditions for the initiation of the observed induction of upstream flow swirl at reduced flow rates.
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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:
978-0-7918-7890-3
PROCEEDINGS PAPER
Flow Analysis in a Spiral Inducer Impeller
J. H. G. Howard,
J. H. G. Howard
University of Waterloo, Waterloo, ON, Canada
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B. R. Hutchinson,
B. R. Hutchinson
Advanced Scientific Computing Ltd., Waterloo, ON, Canada
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R. B. Broberg
R. B. Broberg
Advanced Scientific Computing Ltd., Waterloo, ON, Canada
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J. H. G. Howard
University of Waterloo, Waterloo, ON, Canada
B. R. Hutchinson
Advanced Scientific Computing Ltd., Waterloo, ON, Canada
R. B. Broberg
Advanced Scientific Computing Ltd., Waterloo, ON, Canada
Paper No:
93-GT-227, V03AT15A078; 9 pages
Published Online:
February 25, 2015
Citation
Howard, JHG, Hutchinson, BR, & Broberg, RB. "Flow Analysis in a Spiral Inducer Impeller." Proceedings of the ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition. Volume 3A: General. Cincinnati, Ohio, USA. May 24–27, 1993. V03AT15A078. ASME. https://doi.org/10.1115/93-GT-227
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