Multigrid technique applied to the compressible Euler equations

Kanarachos, A; Vournas, I

dc.contributor.author	Kanarachos, A	en
dc.contributor.author	Vournas, I	en
dc.date.accessioned	2014-03-01T01:09:28Z
dc.date.available	2014-03-01T01:09:28Z
dc.date.issued	1993	en
dc.identifier.issn	0001-5970	en
dc.identifier.uri	https://dspace.lib.ntua.gr/xmlui/handle/123456789/11007
dc.subject	Compressible Euler Equation	en
dc.subject	Multigrid Method	en
dc.subject	Supersonic Flow	en
dc.subject.classification	Mechanics	en
dc.subject.other	NAVIER-STOKES EQUATIONS	en
dc.subject.other	IMPLICIT	en
dc.title	Multigrid technique applied to the compressible Euler equations	en
heal.type	journalArticle	en
heal.identifier.primary	10.1007/BF01173139	en
heal.identifier.secondary	http://dx.doi.org/10.1007/BF01173139	en
heal.language	English	en
heal.publicationDate	1993	en
heal.abstract	An optimized multigrid method (EUFLEX-MG) for the EUFLEX code of MBB is described. The method is based on correction scheme and implicit relaxation procedures and is applied to the two dimensional case. The performance of EUFLEX-MG is demonstrated for subsonic and supersonic flow over a RAE-2822 airfoil and over a NACA-0012 airfoil for a large range of Mach numbers. © 1993 Springer-Verlag.	en
heal.publisher	Springer-Verlag	en
heal.journalName	Acta Mechanica	en
dc.identifier.doi	10.1007/BF01173139	en
dc.identifier.isi	ISI:A1993KC31000002	en
dc.identifier.volume	97	en
dc.identifier.issue	1-2	en
dc.identifier.spage	23	en
dc.identifier.epage	40	en