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dc.contributor.authorKreuzová, Terezie-
dc.date.accessioned2024-07-07T18:43:32Z-
dc.date.available2024-07-07T18:43:32Z-
dc.date.issued2024-
dc.identifier.citationApplied and Computational Mechanics. 2024, vol. 18, no. 1, p. 65-76.en
dc.identifier.issn1802-680X (Print)
dc.identifier.issn2336-1182 (Online)
dc.identifier.urihttp://hdl.handle.net/11025/55655
dc.format12 s.cs
dc.format.mimetypeapplication/pdf
dc.language.isoenen
dc.publisherUniversity of West Bohemiaen
dc.rightsUniversity of West Bohemia. All rights reserved.en
dc.subjecttransonický tokcs
dc.subjectrázová vlnacs
dc.subjectISO 9300cs
dc.titleTransonic flow field in critical flow Venturi nozzleen
dc.typečlánekcs
dc.typearticleen
dc.rights.accessopenAccessen
dc.type.versionpublishedVersionen
dc.description.abstract-translatedIn this paper, theoretical and numerical analysis of a~transonic flow field of critical flow Venturi nozzles according to the ISO~9300 standard is performed. Deviations of the flow field from an estimate based on one dimensionality are clarified. While the theoretical analysis allows prediction of these deviations, the numerical analysis allows quantification of their influence. The main studied phenomena include the local supersonic compression in transonic expansion and the Prandtl-Meyer expansion. The tendency of the flow field to spatial oscillations is shown, alongside the ability of the system to damp these oscillations.en
dc.subject.translatedtransonic flowen
dc.subject.translatedshock waveen
dc.subject.translatedISO 9300en
dc.identifier.doihttps://doi.org/10.24132/acm.2024.880
dc.type.statusPeer revieweden
Appears in Collections:Volume 18, number 1 (2024)
Volume 18, number 1 (2024)

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