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Design and qualification of a supersonic wind tunnel for induced boundary layer transition research
| dc.contributor.author | Bottini, Henny |
| dc.contributor.author | Paniagua, Guillermo |
| dc.contributor.author | Schreivogel, Peter |
| dc.contributor.author | Sonda, Alberto |
| dc.contributor.author | Heras Jiménez, Salvador Augusto de las |
| dc.contributor.other | Universitat Politècnica de Catalunya. Departament de Mecànica de Fluids |
| dc.date.accessioned | 2016-01-19T16:27:10Z |
| dc.date.available | 2016-01-19T16:27:10Z |
| dc.date.issued | 2015-03-01 |
| dc.identifier.citation | Bottini, 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.issn | 0954-4100 |
| dc.identifier.uri | http://hdl.handle.net/2117/81695 |
| dc.description.abstract | This 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.extent | 17 p. |
| dc.language.iso | eng |
| dc.subject | Àrees temàtiques de la UPC::Enginyeria mecànica::Mecànica de fluids |
| dc.subject | Àrees temàtiques de la UPC::Física |
| dc.subject.lcsh | Boundary layer |
| dc.subject.lcsh | Wind tunnels |
| dc.subject.other | supersonic flow |
| dc.subject.other | wind tunnel qualification |
| dc.subject.other | freestream fluctuations |
| dc.subject.other | boundary layer transition |
| dc.subject.other | measurement techniques |
| dc.title | Design and qualification of a supersonic wind tunnel for induced boundary layer transition research |
| dc.type | Article |
| dc.subject.lemac | Capa límit (Dinàmica de fluids) |
| dc.subject.lemac | Túnels aerodinàmics |
| dc.contributor.group | Universitat Politècnica de Catalunya. SIC - Sistemes Intel·ligents de Control |
| dc.identifier.doi | 10.1177/0954410014537612 |
| dc.description.peerreviewed | Peer Reviewed |
| dc.relation.publisherversion | http://pig.sagepub.com/content/229/3/562.abstract |
| dc.rights.access | Open Access |
| local.identifier.drac | 15571619 |
| dc.description.version | Postprint (author's final draft) |
| local.citation.author | Bottini, H.; Paniagua, G.; Schreivogel, P.; Sonda, A.; De Las Heras, S.A. |
| local.citation.publicationName | Proceedings of the Institution of Mechanical Engineers. Part G, journal of aerospace engineering |
| local.citation.volume | 229 |
| local.citation.number | 3 |
| local.citation.startingPage | 562 |
| local.citation.endingPage | 578 |
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