Shock-boundary layer interaction control, predictions using a viscous-inviscid interaction procedure and a navier-stokes solver

Simandirakis, G; Bouras, B; Papailiou, KD

dc.contributor.author	Simandirakis, G	en
dc.contributor.author	Bouras, B	en
dc.contributor.author	Papailiou, KD	en
dc.date.accessioned	2014-03-01T01:13:21Z
dc.date.available	2014-03-01T01:13:21Z
dc.date.issued	1997	en
dc.identifier.issn	10032169	en
dc.identifier.uri	https://dspace.lib.ntua.gr/xmlui/handle/123456789/12437
dc.subject	Passive control	en
dc.subject	Shock/boundary layer interaction	en
dc.subject	Transonic airfoils	en
dc.title	Shock-boundary layer interaction control, predictions using a viscous-inviscid interaction procedure and a navier-stokes solver	en
heal.type	journalArticle	en
heal.identifier.primary	10.1007/s11630-997-0023-4	en
heal.identifier.secondary	http://dx.doi.org/10.1007/s11630-997-0023-4	en
heal.publicationDate	1997	en
heal.abstract	The present contribution describes two prediction methods for flows around transonic airfoils, including shock control devices. The whole work was done in the frame of the European Shock Control Investigation Project EUROSHOCK-AER-2, and the global objective was the improvement of the flight performance, in transonic speed, in terms of cruise speed, fuel consumption and exhaust emissions for both laminar and turbulent wings. More specifically the ""passive"" control of shock/boundary layer interaction, whereby part of the solid surface of the airfoil is replaced by a porous surface over a shallow cavity, has been shown to be a means of improving the aerodynamic characteristics of supercritical airfoils.	en
heal.journalName	Journal of Thermal Science	en
dc.identifier.doi	10.1007/s11630-997-0023-4	en
dc.identifier.volume	6	en
dc.identifier.issue	2	en
dc.identifier.spage	97	en
dc.identifier.epage	110	en