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dc.contributor.authorFonn, Eivind
dc.contributor.authorBrummelen, Harald van
dc.contributor.authorKvamsdal, Trond
dc.contributor.authorRasheed, Adil
dc.date.accessioned2019-02-25T09:49:41Z
dc.date.available2019-02-25T09:49:41Z
dc.date.created2019-01-09T18:33:14Z
dc.date.issued2018
dc.identifier.citationComputer Methods in Applied Mechanics and Engineering. 2018, 346 486-512.nb_NO
dc.identifier.issn0045-7825
dc.identifier.urihttp://hdl.handle.net/11250/2587168
dc.description.abstractReduced-basis methods (RB methods or RBMs) form one of the most promising techniques to deliver numerical solutions of parametrized PDEs in real-time with reasonable accuracy. For incompressible flow problems, RBMs based on LBB stable velocity–pressure spaces do not generally inherit the stability of the underlying high-fidelity model and, instead, additional stabilization techniques must be introduced. One way of bypassing the loss of LBB stability in the RBM is to inflate the velocity space with supremizer modes. This however deteriorates the performance of the RBM in the performance-critical online stage, as additional DOFs must be introduced to retain stability, while these DOFs do not effectively contribute to accuracy of the RB approximation. In this work we consider a velocity-only RB approximation, exploiting a solenoidal velocity basis. The solenoidal reduced basis emerges directly from the high-fidelity velocity solutions in the offline stage. By means of Piola transforms, the solenoidality of the velocity space is retained under geometric transformations, making the proposed RB method suitable also for the investigation of geometric parameters. To ensure exact solenoidality of the high-fidelity velocity solutions that constitute the RB, we consider approximations based on divergence-conforming compatible B-splines. We show that the velocity-only RB method leads to a significant improvement in computational efficiency in the online stage, and that the pressure solution can be recovered a posteriori at negligible extra cost. We illustrate the solenoidal RB approach by modeling steady two-dimensional Navier–Stokes flow around a NACA0015 airfoil at various angles of attack.nb_NO
dc.language.isoengnb_NO
dc.publisherElseviernb_NO
dc.rightsAttribution-NonCommercial-NoDerivatives 4.0 Internasjonal*
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/4.0/deed.no*
dc.titleFast divergence-conforming reduced basis methods for steady Navier–Stokes flownb_NO
dc.typeJournal articlenb_NO
dc.typePeer reviewednb_NO
dc.description.versionpublishedVersionnb_NO
dc.source.pagenumber486-512nb_NO
dc.source.volume346nb_NO
dc.source.journalComputer Methods in Applied Mechanics and Engineeringnb_NO
dc.identifier.doi10.1016/j.cma.2018.11.038
dc.identifier.cristin1653615
dc.description.localcodec ⃝2018The Author(s).Publishedby Elsevier B.V.This is an open access article under the CCBY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).nb_NO
cristin.unitcode194,63,15,0
cristin.unitnameInstitutt for matematiske fag
cristin.ispublishedtrue
cristin.fulltextoriginal
cristin.qualitycode2


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Attribution-NonCommercial-NoDerivatives 4.0 Internasjonal
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