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International Journal of Rotating Machinery
Volume 2019, Article ID 7415263, 12 pages
https://doi.org/10.1155/2019/7415263
Research Article

CFD Modelling of a Centrifugal Compressor with Experimental Validation through Radial Diffuser Static Pressure Measurement

1Business Edge, 6 Dragoon House, Hussar Court, Westside View, Waterlooville, Hants, PO7 7SF, UK
2School of Mechanical and Design Engineering, University of Portsmouth, Anglesea Building, Portsmouth PO1 3DJ, UK
3School of Energy Systems, LUT University, P.O. Box 20, FI-53851 Lappeenranta, Finland

Correspondence should be addressed to Brett Dewar; moc.liamg@1rawedtterb

Received 15 January 2019; Revised 10 April 2019; Accepted 15 April 2019; Published 19 May 2019

Academic Editor: Ryoichi Samuel Amano

Copyright © 2019 Brett Dewar et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

Abstract

This paper compares experimental static pressure measurement with CFD simulation in a centrifugal compressor at 12 points through the diffuser. Three mass flow rates are selected, each for three operating speeds giving nine total operating conditions. The results show that the CFD model generally slightly underpredicts the static pressure value as compared to the experimental results. The discrepancy between experimental and numerical results ranges between -8% and +6% and is fairly consistent for a given operating condition, except for close to the blade trailing edge where the pressure variation is less regular and where the pressure is increasing most rapidly with radial position. In the consistent region, where the pressure gradient is low, the discrepancy is around two percent or less for simulations close to the design operating point. Away from the design operating point the errors increase up to approximately 5%. The simulation results were also used to investigate the effect of the position (from the blade trailing edge) of the impeller-diffuser interface (a characteristic of the frozen rotor simulation approach). Here an optimal position for the interface was found to be 2% of the blade radius. This value gave improved agreement with the experimental result in the initial region of the diffuser up to a distance of approximately 10% of the radius. At greater distances the position of the interface became less important. The results also highlighted a change in the pressure along the spanwise direction close to the tips. A dip in the pressure, which was observed in the experimental results, was only observed in the simulations close to the shroud. Close to the hub the simulation results recorded a small local peak. The simulation approach was then applied to further study the flow characteristics by examining the full-field velocity and pressure contours in the impeller and diffuser regions to identify changes due to the different operating conditions.