Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/116448
DC FieldValueLanguage
dc.contributorDepartment of Civil and Environmental Engineeringen_US
dc.contributorMainland Development Officeen_US
dc.creatorDeng, Een_US
dc.creatorLiu, XYen_US
dc.creatorOuyang, DHen_US
dc.creatorYue, Hen_US
dc.creatorNi, YQen_US
dc.date.accessioned2025-12-30T03:56:45Z-
dc.date.available2025-12-30T03:56:45Z-
dc.identifier.issn0167-6105en_US
dc.identifier.urihttp://hdl.handle.net/10397/116448-
dc.language.isoenen_US
dc.publisherElsevieren_US
dc.subject3D ultrasonic anemometeren_US
dc.subjectHigh-speed trainen_US
dc.subjectIDDESen_US
dc.subjectJet flowen_US
dc.subjectTunnel entranceen_US
dc.title3D ultrasonic anemometer array reveals jet flow structures at the entrance of high-speed railway tunnelen_US
dc.typeJournal/Magazine Articleen_US
dc.identifier.volume257en_US
dc.identifier.doi10.1016/j.jweia.2024.106004en_US
dcterms.abstractHigh-speed trains (HSTs), traveling at speeds of up to 300 km/h, are subjected to safety risks in crosswind conditions, particularly when they enter or exit tunnels due to transient aerodynamic effects. The study employs a three-dimensional (3D) ultrasonic anemometer array positioned at the tunnel entrance to investigate the jet flow structure and its 3D characteristics that are induced by HSTs as they enter tunnels. The main results are as follows: The jet flow speed reaches approximately 3%–7% of the train's operational speed, with a maximum length of around 0.48 L. When the train speed is increased from 300 km/h to 400 km/h, the effect of its slipstream on the surrounding wind speed increases by 33% upon entering the tunnel, while in the jet flow section, the wind speeds from both sources are comparable. Through field measurement and numerical simulation, this study provides better understanding of the characteristics of the 3D jet flow structure generated from HSTs entering tunnels, thus offering more insight in developing means for reducing jet flows.en_US
dcterms.accessRightsembargoed accessen_US
dcterms.bibliographicCitationJournal of wind engineering and industrial aerodynamics, Feb. 2025, v. 257, 106004en_US
dcterms.isPartOfJournal of wind engineering and industrial aerodynamicsen_US
dcterms.issued2025-02-
dc.identifier.scopus2-s2.0-85213860984-
dc.identifier.eissn1872-8197en_US
dc.identifier.artn106004en_US
dc.description.validate202512 bchyen_US
dc.description.oaNot applicableen_US
dc.identifier.SubFormIDG000554/2025-12-
dc.description.fundingSourceOthersen_US
dc.description.fundingTextThis work is funded by the Innovation and Technology Commission of the Hong Kong SAR Government [grant number K-BBY1] and the National Natural Science Foundation of China [grant numbers 52308419].en_US
dc.description.pubStatusPublisheden_US
dc.date.embargo2027-02-28en_US
dc.description.oaCategoryGreen (AAM)en_US
Appears in Collections:Journal/Magazine Article
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Embargo End Date 2027-02-28
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