No AccessComputational Performance of a LES Solver for Supersonic Jet Flow ApplicationsCarlos Junqueira-Junior, Joao Luiz F. Azevedo, Sami Yamouni and William WolfCarlos Junqueira-JuniorAeronautics and Space Institute (IAE)Search for more papers by this author, Joao Luiz F. AzevedoAeronautics and Space Institute (IAE)Search for more papers by this author, Sami YamouniTechnological Institute of Aeronautics (ITA)Search for more papers by this author and William WolfUniversity of CampinasSearch for more papers by this authorAIAA 2017-4411Session: Parallel Computing Methodologies IPublished Online:2 Jun 2017https://doi.org/10.2514/6.2017-4411SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for references What's Popular 23rd AIAA Computational Fluid Dynamics Conference 5-9 June 2017Denver, Coloradohttps://doi.org/10.2514/6.2017-4411 CrossmarkInformationCopyright © 2017 by C. Junqueira-Junior, J.L.F. Azevedo, S. Yamouni, and W.R. Wolf. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsAerodynamicsAerospace SciencesComputational Fluid DynamicsConservation of Momentum EquationsEquations of Fluid DynamicsFlow RegimesFluid DynamicsFluid Flow PropertiesFluid MechanicsNumerical AnalysisTurbulenceTurbulence Models KeywordsIncompressible FlowLarge Eddy SimulationHigh Performance ComputingVelocity ProfilesMach NumberAsynchronous CommunicationsNavier Stokes EquationsThermal ConductivityPrandtl NumberParallel AlgorithmDigital Topics Computational Fluid Dynamics