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Resolvent modelling of near-wall coherent structures in turbulent channel flow

dc.contributor.authorAbreu, Leandra I. [UNESP]
dc.contributor.authorCavalieri, André V.G. [UNESP]
dc.contributor.authorSchlatter, Philipp [UNESP]
dc.contributor.authorVinuesa, Ricardo [UNESP]
dc.contributor.authorHenningson, Dan S. [UNESP]
dc.contributor.institutionUniversidade Estadual Paulista (Unesp)
dc.contributor.institutionInstituto Tecnológico de Aeronáutica
dc.contributor.institutionKTH Royal Institute of Technology
dc.date.accessioned2020-12-12T01:35:18Z
dc.date.available2020-12-12T01:35:18Z
dc.date.issued2020-10-01
dc.description.abstractTurbulent channel flow was analysed using direct numerical simulations at friction Reynolds numbers Reτ=180 and 550. The databases were studied using spectral proper orthogonal decomposition (SPOD) to identify dominant near-wall coherent structures, most of which turn out to be streaks and streamwise vortices. Resolvent analysis was used as a theoretical approach to model such structures, as it allows the identification of the optimal forcing and most amplified flow response; the latter may be related to the observed relevant structures obtained by SPOD, especially if the gain between forcing and response is much larger than what is found for suboptimal forcings or if the non-linear forcing is white noise. Results from SPOD and resolvent analysis were compared for several combinations of frequencies and wavenumbers. For both Reynolds numbers, the best agreement between SPOD and resolvent modes was observed for the cases where the lift-up mechanism from resolvent analysis is present, which are also the cases where the optimal resolvent gain is dominant. These results confirm the outcomes in our previous studies (Abreu et al., 2019; Abreu et al., 2020), where we used a DNS database of a pipe flow for the same Reynolds numbers.en
dc.description.affiliationSão Paulo State University (UNESP), Campus of São João da Boa Vista
dc.description.affiliationDivisão de Engenharia Aeronáutica Instituto Tecnológico de Aeronáutica
dc.description.affiliationFLOW Engineering Mechanics KTH Royal Institute of Technology
dc.description.affiliationUnespSão Paulo State University (UNESP), Campus of São João da Boa Vista
dc.description.sponsorshipConselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)
dc.identifierhttp://dx.doi.org/10.1016/j.ijheatfluidflow.2020.108662
dc.identifier.citationInternational Journal of Heat and Fluid Flow, v. 85.
dc.identifier.doi10.1016/j.ijheatfluidflow.2020.108662
dc.identifier.issn0142-727X
dc.identifier.scopus2-s2.0-85089533954
dc.identifier.urihttp://hdl.handle.net/11449/199271
dc.language.isoeng
dc.relation.ispartofInternational Journal of Heat and Fluid Flow
dc.sourceScopus
dc.subjectCoherent structures
dc.subjectResolvent analysis
dc.subjectSPOD
dc.subjectWall-bounded turbulence
dc.titleResolvent modelling of near-wall coherent structures in turbulent channel flowen
dc.typeArtigopt
dspace.entity.typePublication
unesp.campusUniversidade Estadual Paulista (UNESP), Faculdade de Engenharia, São João da Boa Vistapt

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