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dc.contributor.authorSemlitsch, Bernhard
dc.contributor.authorMihǎescu, M
dc.date.accessioned2019-01-05T00:30:13Z
dc.date.available2019-01-05T00:30:13Z
dc.date.issued2018-12
dc.identifier.issn0001-1452
dc.identifier.urihttps://www.repository.cam.ac.uk/handle/1810/287542
dc.description.abstractScreening numerically internal fluidic injection scenarios for the manipulation of the double diamond shock pattern in convergent-divergent nozzle exhausts, we demonstrate the individual importance of design parameters. We find that the evolving shock pattern is sensitive to the injection location, while the persistence of the induced counterrotating vortex pairs is primarily governed by the injection pressure. Injection close to the nozzle exit generates secondary vortical structures amplifying the fluctuations in the nozzle vicinity.
dc.publisherAmerican Institute of Aeronautics and Astronautics (AIAA)
dc.titleFluidic injection scenarios for shock pattern manipulation in exhausts
dc.typeArticle
prism.endingPage4644
prism.issueIdentifier12
prism.publicationDate2018
prism.publicationNameAIAA Journal
prism.startingPage4640
prism.volume56
dc.identifier.doi10.17863/CAM.34852
dcterms.dateAccepted2018-08-04
rioxxterms.versionofrecord10.2514/1.J057537
rioxxterms.versionAM
rioxxterms.licenseref.urihttp://www.rioxx.net/licenses/all-rights-reserved
rioxxterms.licenseref.startdate2018-12-01
dc.contributor.orcidSemlitsch, Bernhard [0000-0001-7715-863X]
dc.identifier.eissn1533-385X
rioxxterms.typeJournal Article/Review
rioxxterms.freetoread.startdate2019-12-31


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