Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/110037
DC FieldValueLanguage
dc.contributorDepartment of Civil and Environmental Engineering-
dc.contributorMainland Development Office-
dc.creatorLiu, YK-
dc.creatorWang, YL-
dc.creatorDeng, E-
dc.creatorNi, YQ-
dc.creatorYang, WC-
dc.creatorAo, WK-
dc.date.accessioned2024-11-20T07:30:58Z-
dc.date.available2024-11-20T07:30:58Z-
dc.identifier.issn2096-2754-
dc.identifier.urihttp://hdl.handle.net/10397/110037-
dc.language.isoenen_US
dc.publisherKeAi Publishing Communications Ltd.en_US
dc.rights© 2024 Tongji University. Publishing services by Elsevier B.V. on behalf of KeAi Communications Co. Ltd. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).en_US
dc.rightsThe following publication Liu, Y.-K., Wang, Y.-L., Deng, E., Ni, Y.-Q., Yang, W.-C., & Ao, W.-K. (2024). Characteristics of the crack tip field in high-speed railway tunnel linings under train-induced aerodynamic shockwaves. Underground Space, 18, 199-217 is available at https://doi.org/10.1016/j.undsp.2024.01.001.en_US
dc.subjectAerodynamic shockwaveen_US
dc.subjectCrack tip fielden_US
dc.subjectFalling concrete blocksen_US
dc.subjectIntensification effecten_US
dc.subjectStress intensity factoren_US
dc.subjectTunnel lining cracksen_US
dc.titleCharacteristics of the crack tip field in high-speed railway tunnel linings under train-induced aerodynamic shockwavesen_US
dc.typeJournal/Magazine Articleen_US
dc.identifier.spage199-
dc.identifier.epage217-
dc.identifier.volume18-
dc.identifier.doi10.1016/j.undsp.2024.01.001-
dcterms.abstractHigh-speed railway tunnels in various countries have continuously reported accidents of vault falling concrete blocks. Once the concrete block falling occurs, serious consequences follow, and traffic safety may be endangered. The aerodynamic shockwave evolves from the initial compression wave may be an important inducement causing the tunnel lining cracks to grow and form falling concrete blocks. A joint calculation framework is established based on ANSYS Fluent, ABAQUS, and FRANC3D for calculating the crack tip field under the aerodynamic shockwave. The intensification effect of aerodynamic shockwaves in the crack is revealed, and the evolution characteristics of the crack tip field and the influence factors of stress intensity factor (SIF) are analyzed. Results show that (1) the aerodynamic shockwave intensifies after entering the crack, resulting in more significant pressure in the crack than the input pressure. The maximum pressure of the inclined and longitudinal cracks is higher than the corresponding values of the circumferential crack, respectively. (2) The maximum SIF of the circumferential, inclined, and longitudinal crack appears at 0.5, 0.68, and 0.78 times the crack front length. The maximum SIF of the circumferential crack is higher than that of the inclined and longitudinal crack. The possibility of crack growth of the circumferential crack is the highest under aerodynamic shockwaves. (3) The influence of train speed on the SIF of the circumferential crack is more than 40%. When the train speed, crack depth, and crack length change, the change of pressure in the crack is the direct cause of the change of SIF.-
dcterms.accessRightsopen accessen_US
dcterms.bibliographicCitationUnderground space, Oct. 2024, v. 18, p. 199-217-
dcterms.isPartOfUnderground space-
dcterms.issued2024-10-
dc.identifier.scopus2-s2.0-85194937805-
dc.identifier.eissn2467-9674-
dc.description.validate202411 bcch-
dc.description.oaVersion of Recorden_US
dc.identifier.FolderNumberOA_Scopus/WOSen_US
dc.description.fundingSourceOthersen_US
dc.description.fundingTextNational Natural Science Foundation of China; Science and Technology Research and Development Program of China railway group limited; Fundamental Research Funds for the Central Universities of Central South University; Guangdong Basic and Applied Basic Research Foundation Project; Innovation and Technology Commission of Hong Kong, China; Hong Kong Polytechnic University’s Postdoc Matching Fund Schemeen_US
dc.description.pubStatusPublisheden_US
dc.description.oaCategoryCCen_US
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