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dc.contributor.authorFernandez, P.
dc.contributor.authorNguyen, N.C.
dc.contributor.authorRoca, Xevi
dc.contributor.authorPeraire, J.
dc.contributor.otherBarcelona Supercomputing Center
dc.identifier.citationFernandez, P. [et al.]. Implicit large-eddy simulation of compressible flows using the Interior Embedded Discontinuous Galerkin method. A: 54th AIAA Aerospace Sciences Meeting San Diego, California, USA. "54th AIAA Aerospace Sciences Meeting, AIAA SciTech Forum, (AIAA 2016-1332)". 2016.
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.
dc.description.sponsorshipThe first author would like to acknowledge “la Caixa” Foundation for the Graduate Studies Fellowship that support his work. We also gratefully acknowledge Pratt & Whitney and the Air Force Office of Scientific Research for partially supporting this effort. The work of the third author is supported by the European Comission through the Marie Sklodowska-Curie Actions (HiPerMeGaFlowS project). Finally, we would like to thank Prof. M. Drela, Dr. M. Sadeghi and H.-M. Shang for their useful comments and suggestions, and Dr. C. Hill for providing with the computing resources to perform some of the simulations presented in this paper.
dc.format.extent15 p.
dc.subjectÀrees temàtiques de la UPC::Informàtica
dc.subject.lcshSimulation and Modeling
dc.subject.otherImplicit large-eddy simkulation (ILES)
dc.subject.otherDirect numerical simulation (DNS)
dc.subject.otherSGS model
dc.titleImplicit large-eddy simulation of compressible flows using the Interior Embedded Discontinuous Galerkin method
dc.typeConference lecture
dc.subject.lemacSimulació per ordinador
dc.rights.accessOpen Access
dc.description.versionPostprint (published version)
dc.relation.projectidinfo:eu-repo/grantAgreement/EC/H2020/658853/EU/High-Performance Curved Meshing and Unstructured High-Order Galerkin Solvers for High-Fidelity Flow Simulation/HiPerMeGaFlowS
local.citation.contributor54th AIAA Aerospace Sciences Meeting San Diego, California, USA
local.citation.publicationName54th AIAA Aerospace Sciences Meeting, AIAA SciTech Forum, (AIAA 2016-1332)

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