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

Sotiropoulos, F; Alkalai, K; Giannakoglou, K; Papailiou, KD

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