Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/107616
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dc.contributorDepartment of Civil and Environmental Engineeringen_US
dc.creatorGao, Hen_US
dc.creatorLiu, Ten_US
dc.creatorLiu, Zen_US
dc.creatorHuo, Xen_US
dc.creatorZhang, Jen_US
dc.creatorWang, Xen_US
dc.creatorChen, Zen_US
dc.date.accessioned2024-07-04T08:49:09Z-
dc.date.available2024-07-04T08:49:09Z-
dc.identifier.issn0263-2241en_US
dc.identifier.urihttp://hdl.handle.net/10397/107616-
dc.language.isoenen_US
dc.publisherElsevier BVen_US
dc.rights© 2023 Elsevier Ltd. All rights reserved.en_US
dc.rights© 2023. This manuscript version is made available under the CC-BY-NC-ND 4.0 license https://creativecommons.org/licenses/by-nc-nd/4.0/en_US
dc.rightsThe following publication Gao, H., Liu, T., Liu, Z., Huo, X., Zhang, J., Wang, X., & Chen, Z. (2023). Discrete integration for measuring aerodynamic loads on trains in crosswinds − realizable strategies of discretization and discrete integration. Measurement, 216, 112967 is available at https://doi.org/10.1016/j.measurement.2023.112967.en_US
dc.subjectAerodynamic load coefficientsen_US
dc.subjectCrosswindsen_US
dc.subjectDiscrete integrationen_US
dc.subjectDiscretizationen_US
dc.subjectLagrange rectangular elementsen_US
dc.subjectSurface pressure distributionsen_US
dc.titleDiscrete integration for measuring aerodynamic loads on trains in crosswinds - realizable strategies of discretization and discrete integrationen_US
dc.typeJournal/Magazine Articleen_US
dc.identifier.volume216en_US
dc.identifier.doi10.1016/j.measurement.2023.112967en_US
dcterms.abstractDiscrete integration occupies an important place in train aerodynamic tests in crosswinds. Improved delayed detached eddy simulations based on shear stress transport k-ω turbulence models were carried out to calculate the side force, lift, rolling moment around the lee rail, and surface pressure on bluff and streamlined vehicles. The changepoints and piecewise linearities of the pressure coefficients were evaluated, and the maximum coefficient of determination in the elements was 0.9973. A realizable strategy of the discretization based on the Lagrange rectangular elements was suggested, including the largest lengths and numbers of the elements. From this, a strategy of the discrete integration was presented to measure the aerodynamic loads, considering the real orientation of the elements. The maximum errors of the mean aerodynamic load coefficients of the bluff and streamlined vehicles were 4.1% and 2.2% (except the mean lift coefficient of the bluff vehicle), respectively. The errors were less than those in the previous studies, especially for the streamlined vehicle, which reduced by up to 8.7%. The unsteady aerodynamic loads with no delay obtained by the strategies were near to natural ones in the frequency range that people would be concerned about in crosswinds (at the Strouhal number of less than 0.4). Some suggestions were made for using the strategies in the full-scale tests and model tests, which provided a foundation for further studies of the running safety in natural crosswinds.en_US
dcterms.accessRightsopen accessen_US
dcterms.bibliographicCitationMeasurement : Journal of the International Measurement Confederation, July 2023, v. 216, 112967en_US
dcterms.isPartOfMeasurement : Journal of the International Measurement Confederationen_US
dcterms.issued2023-07-
dc.identifier.scopus2-s2.0-85156210743-
dc.identifier.eissn1873-412Xen_US
dc.identifier.artn112967en_US
dc.description.validate202407 bcchen_US
dc.description.oaAccepted Manuscripten_US
dc.identifier.FolderNumbera2947-
dc.identifier.SubFormID48893-
dc.description.fundingSourceSelf-fundeden_US
dc.description.pubStatusPublisheden_US
dc.description.oaCategoryGreen (AAM)en_US
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