No AccessHigh-temperature gas effects at a capsule under re-entry and wind-tunnel conditionsChristian Stemmer and Jonas FehnChristian StemmerTechnical University of MunichSearch for more papers by this author and Jonas FehnTechnical University of MunichSearch for more papers by this authorAIAA 2014-2645Session: Hypersonic Boundary Layer Transition IIPublished Online:13 Jun 2014https://doi.org/10.2514/6.2014-2645SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byRoughness-Induced Boundary-Layer Transition on a Hypersonic Capsule-Like Forebody Including NonequilibriumAntonio Di Giovanni and Christian Stemmer26 August 2019 | Journal of Spacecraft and Rockets, Vol. 56, No. 6Roughness-Induced Crossflow-Type Instabilities in a Hypersonic Capsule Boundary Layer Including NonequilibriumAntonio Di Giovanni and Christian Stemmer27 March 2019 | Journal of Spacecraft and Rockets, Vol. 56, No. 5Cross-flow-type breakdown induced by distributed roughness in the boundary layer of a hypersonic capsule configuration5 October 2018 | Journal of Fluid Mechanics, Vol. 856Numerical Simulations of the High-Enthalpy Boundary Layer on a Generic Capsule Geometry with Roughness31 October 2017 What's Popular 44th AIAA Fluid Dynamics Conference 16-20 June 2014Atlanta, GAhttps://doi.org/10.2514/6.2014-2645 CrossmarkInformationCopyright © 2014 by Christian Stemmer and Jonas Fehn. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsAerodynamic PerformanceAerodynamicsBoundary LayersComputational Fluid DynamicsConservation of Momentum EquationsEquations of Fluid DynamicsFlow RegimesFluid DynamicsFluid Flow PropertiesVortex DynamicsWind Tunnels KeywordsWind Tunnel ModelsPerfect GasThermodynamic PropertiesFree Stream VelocityThermal Boundary Layer ThicknessStagnation PointFlow ConditionsAngle of AttackHeat TransferParabolized Stability EquationsPDF Topics Aerodynamics, Fluids and Thermal Sciences