Internal flows of a low specific speed pump stage, having a mixed-flow impeller and a vaned bowl diffuser combination, have been investigated experimentally and numerically. Air was used as the test fluid, and the internal flows were measured at various locations and under various capacities. Flow calculations were made, for both the isolated impeller case and the complete stage case, using Denton viscous codes LOSS3D and MULTSTAGE14, by which the three-dimensional steady flow through multiple blade rows can be calculated using the inter-row mixing process. Experimental results showed the effects of the interaction between the impeller and the reverse flow, originating in the downstream diffuser, even at the design point capacity. While an impeller exit reverse flow occurred at the shroud side in the isolated impeller calculation, it was observed at the hub side in the complete stage case, showing good agreement with the experimental results. Although the flow in the diffuser was highly distorted due to a strong swirl flow, patterns of total pressure distribution could be well predicted by the complete stage calculation.
Skip Nav Destination
ASME 1994 International Gas Turbine and Aeroengine Congress and Exposition
June 13–16, 1994
The Hague, Netherlands
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7883-5
PROCEEDINGS PAPER
Experimental and Numerical Study of Three-Dimensional Flows in a Mixed-Flow Pump Stage
T. Takemura,
T. Takemura
Ebara Research Company, Limited, Fujisawa-shi, Japan
Search for other works by this author on:
A. Goto
A. Goto
Ebara Research Company, Limited, Fujisawa-shi, Japan
Search for other works by this author on:
T. Takemura
Ebara Research Company, Limited, Fujisawa-shi, Japan
A. Goto
Ebara Research Company, Limited, Fujisawa-shi, Japan
Paper No:
94-GT-044, V001T01A013; 10 pages
Published Online:
February 18, 2015
Citation
Takemura, T, & Goto, A. "Experimental and Numerical Study of Three-Dimensional Flows in a Mixed-Flow Pump Stage." Proceedings of the ASME 1994 International Gas Turbine and Aeroengine Congress and Exposition. Volume 1: Turbomachinery. The Hague, Netherlands. June 13–16, 1994. V001T01A013. ASME. https://doi.org/10.1115/94-GT-044
Download citation file:
231
Views
Related Proceedings Papers
Related Articles
Parametric Design of a Waterjet Pump by Means of Inverse Design, CFD Calculations and Experimental Analyses
J. Fluids Eng (March,2010)
Experimental and Numerical Study of Three-Dimensional Flows in a Mixed-Flow Pump Stage
J. Turbomach (July,1996)
A Unified Procedure for the Calculation of Off-Design Performance of Radial Turbomachinery
J. Eng. Power (January,1971)
Related Chapters
Introduction
Design of Mechanical Bearings in Cardiac Assist Devices
Boundary Layer Analysis
Centrifugal Compressors: A Strategy for Aerodynamic Design and Analysis
Dynamic Behavior of Pumping Systems
Pipeline Pumping and Compression Systems: A Practical Approach