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Turbine cascade calculations through a fractional step

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dc.contributor.author Giannakoglou, K en
dc.contributor.author Simandirakis, G en
dc.contributor.author Papailiou, KD en
dc.date.accessioned 2014-03-01T02:48:05Z
dc.date.available 2014-03-01T02:48:05Z
dc.date.issued 1991 en
dc.identifier.issn 04021215 en
dc.identifier.uri https://dspace.lib.ntua.gr/xmlui/handle/123456789/33516
dc.relation.uri http://www.scopus.com/inward/record.url?eid=2-s2.0-0025749092&partnerID=40&md5=05e54f8b1c30c279fd2e78d5722704fd en
dc.subject.other Computer Software - Applications en
dc.subject.other Mathematical Techniques - Algorithms en
dc.subject.other Fractional Step Navier Stokes Method en
dc.subject.other Software Package Athena en
dc.subject.other Turbine Cascade Flows en
dc.subject.other Two-Layer Baldwin-Lomax Algebraic Turbulent Model en
dc.subject.other Gas Turbines en
dc.title Turbine cascade calculations through a fractional step en
heal.type conferenceItem en
heal.publicationDate 1991 en
heal.abstract An explicit, finite-difference, fractional-step Navier-Stokes method is presented for the prediction of two-dimensional turbomachinery cascade flows. The method also accounts for three-dimensional effects due to radius and streamtube thickness variations. The two-layer Baldwin-Lomax algebraic turbulent model is used to effect closure and its practical implementation is discussed in detail. Three different flow problems are examined and compared with experimental and numerical results obtained elsewhere. These cases deal with transonic flows in the last stage of a steam turbine rotor and a low solidity turbine cascade, as well as the subsonic flow around an isolated RAE2822 profile. The latter case was used for comparing two different transition criteria, implemented in the present code. C-type computational grids are used which are quasiorthogonal in the near wall region. en
heal.publisher Publ by ASME, New York, NY, United States en
heal.journalName American Society of Mechanical Engineers (Paper) en


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