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dc.contributor.authorSerkov, S. A.en
dc.contributor.authorSedunin, V. A.en
dc.contributor.authorBlinov, V. L.en
dc.contributor.authorKomarov, O. V.en
dc.contributor.authorBrodov, Y. M.en
dc.date.accessioned2020-09-29T09:46:42Z-
dc.date.available2020-09-29T09:46:42Z-
dc.date.issued2020-
dc.identifier.citationIdentification of corner separation modelling in axial compressor stage / S. A. Serkov, V. A. Sedunin, V. L. Blinov, O. V. Komarov, et al. . — DOI 10.1051/e3sconf/202017801035 // E3S Web of Conferences. — 2020. — Iss. 178. — 1035.en
dc.identifier.issn2555-0403-
dc.identifier.otherhttps://www.e3s-conferences.org/articles/e3sconf/pdf/2020/38/e3sconf_hsted2020_01035.pdfpdf
dc.identifier.other1good_DOI
dc.identifier.other32ace364-e262-4837-ab1c-21e18864f4ddpure_uuid
dc.identifier.otherhttp://www.scopus.com/inward/record.url?partnerID=8YFLogxK&scp=85089535302m
dc.identifier.urihttp://elar.urfu.ru/handle/10995/90272-
dc.description.abstractThe paper presents a study of corner separations in hub to blade region at various operation conditions towards compressor stall. It is known that for compressor flows with low or none separations computation fluid dynamics with RANS methods work quite well, however, for highly separated flows they are no longer entirely valid. Therefore, several criteria were applied for prediction and quantification of possible corner separation, and the main interest of this work is in predicting the separation just before it will actually happen by certain flow metrics, so these metrics can be further used as a 'pre-stall' criteria whilst the RANS CFD operating point still behave within its appropriate limits. Also the effect of shear lean is discussed in the presented context. © The Authors, published by EDP Sciences, 2020.en
dc.format.mimetypeapplication/pdfen
dc.language.isoenen
dc.publisherEDP Sciencesen
dc.rightsinfo:eu-repo/semantics/openAccessen
dc.rightscc-byother
dc.sourceE3S Web of Conferencesen
dc.subjectAXIAL-FLOW COMPRESSORSen
dc.subjectCOMPUTATIONAL FLUID DYNAMICSen
dc.subjectNAVIER STOKES EQUATIONSen
dc.subjectAXIAL COMPRESSORSen
dc.subjectCOMPRESSOR FLOWen
dc.subjectCOMPUTATION FLUID DYNAMICSen
dc.subjectCORNER SEPARATIONen
dc.subjectOPERATING POINTSen
dc.subjectOPERATION CONDITIONSen
dc.subjectSEPARATED FLOWSen
dc.subjectSHEAR FLOWen
dc.titleIdentification of corner separation modelling in axial compressor stageen
dc.typeConference Paperen
dc.typeinfo:eu-repo/semantics/conferenceObjecten
dc.typeinfo:eu-repo/semantics/publishedVersionen
dc.identifier.doi10.1051/e3sconf/202017801035-
dc.identifier.scopus85089535302-
local.affiliationUral Federal University, Turbines and Engines Department, Yekaterinburg, 620002, Russian Federationen
local.contributor.employeeSerkov, S.A., Ural Federal University, Turbines and Engines Department, Yekaterinburg, 620002, Russian Federationru
local.contributor.employeeSedunin, V.A., Ural Federal University, Turbines and Engines Department, Yekaterinburg, 620002, Russian Federationru
local.contributor.employeeBlinov, V.L., Ural Federal University, Turbines and Engines Department, Yekaterinburg, 620002, Russian Federationru
local.contributor.employeeKomarov, O.V., Ural Federal University, Turbines and Engines Department, Yekaterinburg, 620002, Russian Federationru
local.contributor.employeeBrodov, Y.M., Ural Federal University, Turbines and Engines Department, Yekaterinburg, 620002, Russian Federationru
local.issue178-
local.identifier.pure13683139-
local.description.order1035-
local.identifier.eid2-s2.0-85089535302-
Располагается в коллекциях:Научные публикации ученых УрФУ, проиндексированные в SCOPUS и WoS CC

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