Experimental Study on Hysteresis during Cavitating Vortex Onset in Pump-as-Turbine Applications
Loading...
Date
Advisor
Referee
Mark
Journal Title
Journal ISSN
Volume Title
Publisher
IOP Publishing
Altmetrics
Abstract
Centrifugal pumps operating in turbine mode (pump-as-turbine) have become a relatively common solution for small-scale hydropower plants and for energy recovery applications. One of the aspects of pump-as-turbine (PaT) operation is that the pump impeller is generally designed for exclusive operation in pump mode. Therefore, significant residual swirl exits the impeller in turbine mode and creates a dominant swirling motion in the discharge pipe. The magnitude of this swirling flow depends on the operating mode of the PaT. Due to inconvenient blade angles, the swirling motion with coherent vortices might be the dominant component even under the best efficiency operating conditions. The present study focuses on the experimental analysis of the cavitating vortex developed downstream in the discharge pipe. The effect of hysteresis on vortex dynamics is assessed with regard to increase and decrease of cavitation number. The primary concern is with the frequency and amplitude measured by the pressure sensor downstream of PaT. These results are correlated with the image analysis of the cavitating vortex shape recorded by the high-speed camera. The results indicated that the main source of hysteresis is caused by self-induced instabilities of the cavitating vortex. The description and understanding of this phenomenon is important for further correlation of CFD simulations with measured data and for reliable operation of PaTs.
Description
Keywords
Citation
IOP Conference Series: Earth and Environmental Science. 2025, vol. 1561, p. 1-6.
https://iopscience.iop.org/article/10.1088/1755-1315/1561/1/012017
https://iopscience.iop.org/article/10.1088/1755-1315/1561/1/012017
Document type
Peer-reviewed
Document version
Published version
Date of access to the full text
Language of document
en
Study field
Comittee
Date of acceptance
Defence
Result of defence
Endorsement
Review
Supplemented By
Referenced By
Creative Commons license
Except where otherwised noted, this item's license is described as Creative Commons Attribution 4.0 International

0000-0003-4230-5219 