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dc.contributor.authorDrela, Mark
dc.contributor.authorHuang, Arthur
dc.contributor.authorDarmofal, David
dc.date.accessioned2021-09-20T17:16:56Z
dc.date.available2021-09-20T17:16:56Z
dc.date.issued2020-02-21
dc.identifier.urihttps://hdl.handle.net/1721.1/131405
dc.description.abstractAbstract The paper presents the screened expanding corner vane concept, which can turn a channel flow by $$90^\circ$$90∘, while simultaneously increasing the flow area by at least a factor of two and thus halving the mean velocity, all without incurring any significant flow separation. The concept is demonstrated experimentally, and investigated with analytical and computational models. One target application is an ultra-compact closed-circuit wind tunnel, whose overall length is roughly half that of a conventional wind tunnel with the same test section. Graphic abstracten_US
dc.publisherSpringer Berlin Heidelbergen_US
dc.relation.isversionofhttps://doi.org/10.1007/s00348-020-2910-3en_US
dc.rightsCreative Commons Attribution-Noncommercial-Share Alikeen_US
dc.rights.urihttp://creativecommons.org/licenses/by-nc-sa/4.0/en_US
dc.sourceSpringer Berlin Heidelbergen_US
dc.titleScreened expanding turning-vane concepten_US
dc.typeArticleen_US
dc.identifier.citationExperiments in Fluids. 2020 Feb 21;61(3):75en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.eprint.versionAuthor's final manuscripten_US
dc.type.urihttp://purl.org/eprint/type/JournalArticleen_US
eprint.statushttp://purl.org/eprint/status/PeerRevieweden_US
dc.date.updated2020-09-24T20:55:36Z
dc.language.rfc3066en
dc.rights.holderSpringer-Verlag GmbH Germany, part of Springer Nature
dspace.embargo.termsY
dspace.date.submission2020-09-24T20:55:36Z
mit.licenseOPEN_ACCESS_POLICY
mit.metadata.statusAuthority Work and Publication Information Needed


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