Application of a fractional step algorithm to the solution of inviscid turbomachinery flow problems

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dc.contributor.author Sotiropoulos, F en
dc.contributor.author Alkalai, K en
dc.contributor.author Giannakoglou, K en
dc.contributor.author Papailiou, KD en
dc.date.accessioned 2014-03-01T02:47:50Z
dc.date.available 2014-03-01T02:47:50Z
dc.date.issued 1988 en
dc.identifier.uri https://dspace.lib.ntua.gr/xmlui/handle/123456789/33383
dc.relation.uri http://www.scopus.com/inward/record.url?eid=2-s2.0-0024172382&partnerID=40&md5=0abfcdbdeb4a7bd736752608c657f724 en
dc.subject.other Mathematical Techniques--Algorithms en
dc.subject.other Fractional Step Algorithm en
dc.subject.other Inviscid Two-Dimensional Blade-to-Blade Flow en
dc.subject.other McCormack Explicit Scheme en
dc.subject.other Turbomachinery Flow Problems en
dc.subject.other Turbomachinery en
dc.title Application of a fractional step algorithm to the solution of inviscid turbomachinery flow problems en
heal.type conferenceItem en
heal.publicationDate 1988 en
heal.abstract A fractional step numerical procedure for the solution of inviscid two-dimensional blade-to-blade flow problems is presented. A predictor-corrector McCormack explicit scheme is employed in order to advance the solution within each fractional step. The procedure is enhanced with local time stepping and second order artificial dissipation. Results are presented for channel as well as cascade flows in the subsonic and the transonic flow regimes. en
heal.publisher Publ by American Soc of Mechanical Engineers (ASME), New York, NY, United States en
heal.journalName American Society of Mechanical Engineers, Fluids Engineering Division (Publication) FED en
dc.identifier.volume 69 en
dc.identifier.spage 13 en
dc.identifier.epage 18 en

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