No AccessCartesian Euler Code Application for Launch Vehicle SystemsLes Hall, William Eppard, Michael Applebaum and John BlevinsLes HallCRM Solutions, Inc.Search for more papers by this author, William EppardCRM Solutions, Inc.Search for more papers by this author, Michael ApplebaumCRM Solutions, Inc.Search for more papers by this author and John BlevinsNASA Marshall Space Flight CenterSearch for more papers by this authorPublished Online:14 Jun 2012https://doi.org/10.2514/6.2011-1113SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byAn Overview of the Characterization of the Space Launch System Aerodynamic EnvironmentsJohn A. Blevins, John R. Campbell, David W. Bennett, Russ Rausch, Reynaldo J. Gomez and Cetin C. Kiris10 January 2014 What's Popular 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 04 January 2011 - 07 January 2011Orlando, Floridahttps://doi.org/10.2514/6.2011-1113 Crossmark TopicsAerodynamic PerformanceAerodynamicsAerospace SciencesComputational Fluid DynamicsFEM ElementsFinite Element MethodFluid DynamicsMesh GenerationShock WavesSlip (Aerodynamics)TurbulenceTurbulence ModelsWind Tunnels KeywordsLaunch Vehicle DesignAerodynamic CharacteristicsReynolds Averaged Navier StokesCart3DWind Tunnel TestsCFD SimulationSix Degree of FreedomAngle of AttackNASA Marshall Space Flight CenterDamping CoefficientDigital Submission Topic Aerospace Systems, Operations and Life Cycle
