Design procedure and honeycomb screen implementation to the air transtport department’s subsonic wind tunnel

dc.contributor.authorHrúz, Michal
dc.contributor.authorPecho, Pavol
dc.contributor.authorBugaj, Martin
dc.date.accessioned2021-03-10T10:55:19Z
dc.date.available2021-03-10T10:55:19Z
dc.date.issued2020
dc.description.abstractWind tunnels are the most widely used tools when comes to validation of Reynold number. Most of wind tunnels use various air straighteners or flow conditioners to achieve as most unified air flow as it’s possible. This article deals with design and creation procedure of air flow straightener – honeycomb screen. Based on mathematical relations and empirical experience defines dimensions and characteristics for subsonic wind tunnel of the Air Transport Department of University of Žilina. Wind tunnel equipped with a suitable screen provides more relevant and accurate data, which are crucial for final validation of results of test objects.en_US
dc.identifier.doihttps://doi.org/10.26552/aer.C.2020.2.1
dc.identifier.issn1338-8215
dc.identifier.urihttp://drepo.uniza.sk/handle/hdluniza/406
dc.language.isoenen_US
dc.publisherUniversity of Zilinaen_US
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/
dc.subjecthoneycomben_US
dc.subjectair straighteneren_US
dc.subjectflow conditioneren_US
dc.subjectflow straighteneren_US
dc.subjectscreenen_US
dc.subjectwind tunnelen_US
dc.titleDesign procedure and honeycomb screen implementation to the air transtport department’s subsonic wind tunnelen_US
dc.typeArticleen_US

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