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High-speed flow in an annular cascade with tip clearance: Numerical investigation

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dc.contributor.author Politis, ES en
dc.contributor.author Giannakoglou, KC en
dc.contributor.author Papailiou, KD en
dc.date.accessioned 2014-03-01T02:48:40Z
dc.date.available 2014-03-01T02:48:40Z
dc.date.issued 1998 en
dc.identifier.issn 04021215 en
dc.identifier.uri https://dspace.lib.ntua.gr/xmlui/handle/123456789/34005
dc.relation.uri http://www.scopus.com/inward/record.url?eid=2-s2.0-0031703049&partnerID=40&md5=9abe94f3fa72cb96a34758edee0aa1bf en
dc.subject.other Computational fluid dynamics en
dc.subject.other Computer simulation en
dc.subject.other Flow patterns en
dc.subject.other Mathematical models en
dc.subject.other Navier Stokes equations en
dc.subject.other Reynolds number en
dc.subject.other Turbomachine blades en
dc.subject.other Turbulence en
dc.subject.other Tip clearance effects en
dc.subject.other Turbulence models en
dc.subject.other Cascades (fluid mechanics) en
dc.title High-speed flow in an annular cascade with tip clearance: Numerical investigation en
heal.type conferenceItem en
heal.publicationDate 1998 en
heal.abstract The high-speed flow in an annular cascade with two tip clearance sizes is numerically modeled using a Navier-Stokes solver and the high-Reynolds-number k-ε turbulence model. The numerical predictions should be regarded as complementary to the experimental work conducted in the NTUA annular cascade facility, designed for studying tip-clearance effects in compressor cascades. In the numerically simulated experiment, the stationary blades are mounted on the casing and the tip clearance is formed between them and the spinning hub. The purpose of the present paper is to scrutinize flow trends identified during the measurements and elucidate the flow patterns in the blade passage for rotating and stationary hub. en
heal.publisher ASME, Fairfield, NJ, United States en
heal.journalName American Society of Mechanical Engineers (Paper) en
dc.identifier.issue GT en


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