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dc.contributor.authorGaliana, Francisco J Duráen
dc.contributor.authorWheeler, Andrew PSen
dc.contributor.authorOng, Jonathanen
dc.date.accessioned2016-04-15T11:14:45Z
dc.date.available2016-04-15T11:14:45Z
dc.date.issued2016en
dc.identifier.citationGaliana et al. Journal of Turbomachinery (2016)en
dc.identifier.issn0889-504X
dc.identifier.urihttps://www.repository.cam.ac.uk/handle/1810/254996
dc.description.abstractIn this paper vane trailing-edge losses which occur in Organic Rankine Cycle (ORC) turbines are investigated. Experiments are performed to study the influence of dense gas effects on trailing-edge loss in supersonic flows using a novel Ludwieg tube facility for the study of dense-gas flows. The data is also used to validate a CFD flow solver. The computational simulations are then used to determine the contributions to loss from shocks and viscous effects which occur at the vane trailing-edge. The results show that dense gas effects play a vital role in the structure of the trailing-edge flow, and control the extent of shock and viscous losses.
dc.description.sponsorshipThis work was supported by the EPSRC (EP/J006394/1 and EP/L027437/1) and GE Global Research.
dc.languageEnglishen
dc.language.isoenen
dc.publisherAmerican Society of Mechanical Engineers
dc.titleA study of trailing-edge losses in Organic Rankine Cycle turbinesen
dc.typeConference Object
dc.description.versionThis is the author accepted manuscript. It is currently under an indefinite embargo pending publication by the American Society of Mechanical Engineers.en
prism.publicationDate2016en
dc.rioxxterms.funderEPSRC
dc.rioxxterms.projectidEP/J006394/1
dc.rioxxterms.projectidEP/L027437/1
rioxxterms.versionAM
rioxxterms.licenseref.urihttp://www.rioxx.net/licenses/all-rights-reserveden
rioxxterms.licenseref.startdate2016en
rioxxterms.typeConference Paper/Proceeding/Abstracten
pubs.funder-project-idEPSRC (EP/L027437/1)


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