CERESResearch Repository

Insights into the cavitation behavior of a boundary layer pump

dc.contributor.authorBakogianni, Agapi
dc.contributor.authorRajendran, David John
dc.contributor.authorAnselmi Palma, Eduardo
dc.contributor.authorPachidis, Vassilios
dc.contributor.authorPalmer, Chloe Jo
dc.date.accessioned2026-01-22T11:53:27Z
dc.date.available2026-01-22T11:53:27Z
dc.date.freetoread2026-01-22
dc.date.issued2025-12
dc.date.pubOnline2025-09-24
dc.descriptionCopyright VC 2025 by Rolls-Royce plc.
dc.description.abstractSeveral researchers in literature have claimed that boundary layer pumps have an increased resistance to cavitation because of the absence of blades. Their conclusion was obtained analytically by applying the simple assumption of uniform radial velocity at the entrance of all the channels. This study considers the effect of flow distribution between the channels and assesses the full 3D geometry of a boundary layer pump which was tested in an experimental campaign by Morris. The pump's flow field is obtained with steady-state multiphase 3D-RANS simulations in which the inlet total pressure is gradually reduced. For each inlet total pressure point, the vapor formation is examined, and hence the cavitation mechanisms are analyzed, and the head drop curve is obtained. Results show that the mass flow distribution in the channels is highly nonuniform, which heavily affects vapor formation areas. There is a 127% difference between the lowest and highest channel mass flow. Less mass flow is entering the channels closer to the entrance of the pump, because this requires the flow to turn almost 90 deg from the axial to the radial direction. The viscous forces accelerate less mass more easily, and this leads to up to 22% lower pressure values in the low flow channels. Therefore, vapor starts forming in these channels, and the further the net positive suction head (NPSH) reduces, it sequentially propagates to adjacent channels toward the back like a domino and expands its volume inside each gap.
dc.description.journalNameJournal of Engineering for Gas Turbines and Power
dc.description.sponsorshipCranfield University, Rolls-Royce plc
dc.identifier.citationBakogianni A, Rajendran DJ, Palma EA, et al., (2025) Insights into the cavitation behavior of a boundary layer pump. Journal of Engineering for Gas Turbines and Power, Volume 147, Issue 12, December 2025, Article number 121012en_UK
dc.identifier.eissn1528-8919
dc.identifier.elementsID863061
dc.identifier.issn0742-4795
dc.identifier.issueNo12
dc.identifier.paperNo121012
dc.identifier.urihttps://doi.org/10.1115/1.4069454
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/24816
dc.identifier.volumeNo147
dc.languageEnglish
dc.language.isoen
dc.publisherAmerican Society of Mechanical Engineers (ASME)en_UK
dc.publisher.urihttps://asmedigitalcollection.asme.org/gasturbinespower/article/147/12/121012/1221114/Insights-Into-the-Cavitation-Behavior-of-a
dc.rightsAttribution 4.0 Internationalen
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/
dc.subject4012 Fluid Mechanics and Thermal Engineeringen_UK
dc.subject40 Engineeringen_UK
dc.subjectEnergyen_UK
dc.subject4001 Aerospace engineeringen_UK
dc.subject4004 Chemical engineeringen_UK
dc.titleInsights into the cavitation behavior of a boundary layer pumpen_UK
dc.typeArticle
dc.type.subtypeJournal Article
dcterms.dateAccepted2025-07-16

Files

Original bundle

Now showing 1 - 1 of 1
Loading...
Thumbnail Image
Name:
Insights_Into_the_Cavitation-2025.pdf
Size:
724.74 KB
Format:
Adobe Portable Document Format
Description:
Published version

License bundle

Now showing 1 - 1 of 1
Loading...
Thumbnail Image
Name:
license.txt
Size:
1.63 KB
Format:
Plain Text
Description: