Show simple item record

dc.contributor.authorBottini, Henny
dc.contributor.authorPaniagua, Guillermo
dc.contributor.authorSchreivogel, Peter
dc.contributor.authorSonda, Alberto
dc.contributor.authorHeras Jiménez, Salvador Augusto de las
dc.contributor.otherUniversitat Politècnica de Catalunya. Departament de Mecànica de Fluids
dc.date.accessioned2016-01-19T16:27:10Z
dc.date.available2016-01-19T16:27:10Z
dc.date.issued2015-03-01
dc.identifier.citationBottini, H., Paniagua, G., Schreivogel, P., Sonda, A., De Las Heras, S.A. Design and qualification of a supersonic wind tunnel for induced boundary layer transition research. "Proceedings of the Institution of Mechanical Engineers. Part G, journal of aerospace engineering", 01 Març 2015, vol. 229, núm. 3, p. 562-578.
dc.identifier.issn0954-4100
dc.identifier.urihttp://hdl.handle.net/2117/81695
dc.description.abstractThis paper presents the design and the results of the qualification test campaign of a multiple Mach number supersonic wind tunnel designed for induced boundary layer transition. Its characteristics, function, and instrumentation are described. The range of Mach numbers successfully span is presented along with the measured intensities of freestream fluctuations. All the measurement techniques implemented in the test campaigns after the qualification are introduced, and some results shown and commented to highlight their potentialities.
dc.format.extent17 p.
dc.language.isoeng
dc.subjectÀrees temàtiques de la UPC::Enginyeria mecànica::Mecànica de fluids
dc.subjectÀrees temàtiques de la UPC::Física
dc.subject.lcshBoundary layer
dc.subject.lcshWind tunnels
dc.subject.othersupersonic flow
dc.subject.otherwind tunnel qualification
dc.subject.otherfreestream fluctuations
dc.subject.otherboundary layer transition
dc.subject.othermeasurement techniques
dc.titleDesign and qualification of a supersonic wind tunnel for induced boundary layer transition research
dc.typeArticle
dc.subject.lemacCapa límit (Dinàmica de fluids)
dc.subject.lemacTúnels aerodinàmics
dc.contributor.groupUniversitat Politècnica de Catalunya. SIC - Sistemes Intel·ligents de Control
dc.identifier.doi10.1177/0954410014537612
dc.description.peerreviewedPeer Reviewed
dc.relation.publisherversionhttp://pig.sagepub.com/content/229/3/562.abstract
dc.rights.accessOpen Access
drac.iddocument15571619
dc.description.versionPostprint (author's final draft)
upcommons.citation.authorBottini, H., Paniagua, G., Schreivogel, P., Sonda, A., De Las Heras, S.A.
upcommons.citation.publishedtrue
upcommons.citation.publicationNameProceedings of the Institution of Mechanical Engineers. Part G, journal of aerospace engineering
upcommons.citation.volume229
upcommons.citation.number3
upcommons.citation.startingPage562
upcommons.citation.endingPage578


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record

All rights reserved. This work is protected by the corresponding intellectual and industrial property rights. Without prejudice to any existing legal exemptions, reproduction, distribution, public communication or transformation of this work are prohibited without permission of the copyright holder