No AccessComputational fluid dynamics application to hypersonic flow over a Martian entry vehicle (MEV) - A correlation with experimentJOHN STEWART, ROBERT SMITH and GEORGE ASHBY, JR.JOHN STEWARTComputer Sciences Corp., Hampton, VASearch for more papers by this author, ROBERT SMITHNASA, Langley Research Center, Hampton, VASearch for more papers by this author and GEORGE ASHBY, JR.NASA, Langley Research Center, Hampton, VASearch for more papers by this authorPublished Online:17 Aug 2012https://doi.org/10.2514/6.1992-836SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byComputation of nonequilibrium hypersonic viscous flow about a Martian Entry Vehicle (MEV)S. Tiwari, A. Thomas and R. Smith22 August 2012An adaptive grid method for computing the high speed 3D viscous flowabout a re-entry vehicleMICHAEL BOCKELIE and ROBERT SMITH17 August 2012 What's Popular 30th Aerospace Sciences Meeting and Exhibit 06 January 1992 - 09 January 1992Reno,NV,U.S.A.https://doi.org/10.2514/6.1992-836 Crossmark TopicsAerodynamic PerformanceAerodynamicsAerospace SciencesComputational Fluid DynamicsConservation of Momentum EquationsEquations of Fluid DynamicsFlow RegimesFluid DynamicsFluid Flow PropertiesSkin FrictionWind Tunnels KeywordsCompressible FlowComputational Fluid DynamicsAngle of AttackAerodynamic CharacteristicsNavier Stokes EquationsWind Tunnel ModelsEuler EquationsSurface ModelingLift Over Drag RatioAerobrakingDigital Submission Topic Aerospace Systems, Operations and Life Cycle