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dc.contributor.authorFernandez del Campo, Pablo
dc.contributor.authorNguyen, Ngoc Cuong
dc.contributor.authorRoca, X.
dc.contributor.authorPeraire, Jaime
dc.date.accessioned2016-06-07T14:02:31Z
dc.date.available2016-06-07T14:02:31Z
dc.date.issued2016-01
dc.identifier.isbn978-1-62410-393-3
dc.identifier.urihttp://hdl.handle.net/1721.1/103033
dc.description.abstractWe present a high-order implicit large-eddy simulation (ILES) approach for simulating transitional turbulent flows. The approach consists of an Interior Embedded Discontinuous Galerkin (IEDG) method for the discretization of the compressible Navier-Stokes equations and a parallel preconditioned Newton-GMRES solver for the resulting nonlinear system of equations. The IEDG method arises from the marriage of the Embedded Discontinuous Galerkin (EDG) method and the Hybridizable Discontinuous Galerkin (HDG) method. As such, the IEDG method inherits the advantages of both the EDG method and the HDG method to make itself well-suited for turbulence simulations. We propose a minimal residual Newton algorithm for solving the nonlinear system arising from the IEDG discretization of the Navier-Stokes equations. The preconditioned GMRES algorithm is based on a restricted additive Schwarz (RAS) preconditioner in conjunction with a block incomplete LU factorization at the subdomain level. The proposed approach is applied to the ILES of transitional turbulent flows over a NACA 65-(18)10 compressor cascade at Reynolds number 250,000 in both design and off-design conditions. The high-order ILES results show good agreement with a subgrid-scale LES model discretized with a second-order finite volume code while using significantly less degrees of freedom. This work shows that high-order accuracy is key for predicting transitional turbulent flows without a SGS model.en_US
dc.description.sponsorshipPratt & Whitney Aircraft Companyen_US
dc.description.sponsorshipEuropean Commission (Marie Sklodowska-Curie Actions (HiPerMeGaFlowS project))en_US
dc.description.sponsorshipUnited States. Air Force Office of Scientific Researchen_US
dc.language.isoen_US
dc.publisherAmerican Institute of Aeronautics and Astronautics (AIAA)en_US
dc.relation.isversionofhttp://dx.doi.org/10.2514/6.2016-1332en_US
dc.rightsCreative Commons Attribution-Noncommercial-Share Alikeen_US
dc.rights.urihttp://creativecommons.org/licenses/by-nc-sa/4.0/en_US
dc.sourceProf. Peraireen_US
dc.titleImplicit large-eddy simulation of compressible flows using the Interior Embedded Discontinuous Galerkin methoden_US
dc.typeArticleen_US
dc.identifier.citationFernandez, P., N. C. Nguyen, X.Roca, and J. Peraire. “Implicit Large-Eddy Simulation of Compressible Flows Using the Interior Embedded Discontinuous Galerkin Method.” 54th AIAA Aerospace Sciences Meeting (January 2, 2016).en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronauticsen_US
dc.contributor.approverPablo Fernandezen_US
dc.contributor.mitauthorFernandez del Campo, Pabloen_US
dc.contributor.mitauthorNguyen, Ngoc Cuongen_US
dc.contributor.mitauthorPeraire, Jaimeen_US
dc.relation.journal54th AIAA Aerospace Sciences Meetingen_US
dc.eprint.versionAuthor's final manuscripten_US
dc.type.urihttp://purl.org/eprint/type/ConferencePaperen_US
eprint.statushttp://purl.org/eprint/status/NonPeerRevieweden_US
dspace.orderedauthorsFernandez, Pablo; Nguyen, Cuong; Roca, Xevi; Peraire, Jaimeen_US
dspace.embargo.termsNen_US
dc.identifier.orcidhttps://orcid.org/0000-0002-8556-685X
dc.identifier.orcidhttps://orcid.org/0000-0002-6291-4946
mit.licenseOPEN_ACCESS_POLICYen_US
mit.metadata.statusComplete


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