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dc.contributor.authorJiang, Fengjian
dc.contributor.authorPettersen, Bjørnar
dc.contributor.authorAndersson, Helge Ingolf
dc.date.accessioned2019-09-23T07:47:33Z
dc.date.available2019-09-23T07:47:33Z
dc.date.created2019-09-18T15:11:44Z
dc.date.issued2019
dc.identifier.citationJournal of Fluid Mechanics. 2019, 878 663-699.nb_NO
dc.identifier.issn0022-1120
dc.identifier.urihttp://hdl.handle.net/11250/2618146
dc.description.abstractWe present a detailed study of the turbulent wake behind a quarter-of-ring curved cylinder at Reynolds number Re = 3900 (based on cylinder diamter and incoming ow velocity), by means of Direct Numerical Simulation (DNS). The con guration is referred to as a concave curved cylinder with incoming ow aligned with the plane of curvature and towards the inner face of the cylinder. Wake ows behind this con guration are known to be complex, but have so far only been studied at low Re. This is the rst DNS investigation of the turbulent wake behind the concave con guration, from which we reveal new and interesting wake dynamics, and present in-depth physical interpretations. Similar as in the low-Re cases, the turbulent wake behind a concave curved cylinder is a multi-regime and multi-frequency ow. However, in addition to the co-existing ow regimes reported at lower Re, we observe a new transitional ow regime at Re = 3900. The ow eld in this transitional regime is not dominated by von K arm an-type vortex shedding, but by periodic asymmetric helical vortices. Such vortex pairs exist also in some other wake ows, but are then non-periodic. Inspections reveal that the periodic motion of the asymmetric helical vortices is induced by vortex shedding in its neighboring oblique shedding regime. The oblique shedding regime is in turn in uenced by the transitional regime, resulting in a uni ed and remarkably low dominating frequency in both ow regimes. Due to this synchronized frequency, the new wake dynamics in the transitional regime might easily be overlooked. In the near-wake, two distinct peaks are observed in the time-averaged axial velocity distribution along the curved cylinder span, while only one peak was observed at lower Re. The presence of the additional peak is ascribed to a strong favorable base pressure gradient along the cylinder span. It is noteworthy that the axially-directed base ow exceeded the incoming velocity behind a substantial part of the quarter-of-ring and even persisted upwards along the straight vertical extension. As a by-product of our study, we nd that a straight vertical extension of 16 cylinder diameters is required in order to avoid any adverse e ects from the upper boundary of the ow domain.nb_NO
dc.language.isoengnb_NO
dc.publisherCambridge University Pressnb_NO
dc.titleTurbulent wake behind a concave curved cylindernb_NO
dc.typeJournal articlenb_NO
dc.typePeer reviewednb_NO
dc.description.versionacceptedVersionnb_NO
dc.source.pagenumber663-699nb_NO
dc.source.volume878nb_NO
dc.source.journalJournal of Fluid Mechanicsnb_NO
dc.identifier.doi10.1017/jfm.2019.648
dc.identifier.cristin1726337
dc.description.localcode© 2019. This is the authors’ accepted and refereed manuscript to the article. Locked until 18.3.2020 due to copyright restrictions.nb_NO
cristin.unitcode194,64,20,0
cristin.unitcode194,64,25,0
cristin.unitnameInstitutt for marin teknikk
cristin.unitnameInstitutt for energi- og prosessteknikk
cristin.ispublishedtrue
cristin.qualitycode2


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