No AccessTime-Accurate Simulation of Shock Propagation and Reflection in an Axi-Symmetric Shock TubeMouna Lamnaouer, Alain Kassab, Eduardo Divo, Rodrigo Garza Urquiza, Nolan Polley and Eric PetersenMouna LamnaouerUniversity of Central FloridaSearch for more papers by this author, Alain KassabUniversity of Central FloridaSearch for more papers by this author, Eduardo DivoUniversity of Central FloridaSearch for more papers by this author, Rodrigo Garza UrquizaTexas A&M UniversitySearch for more papers by this author, Nolan PolleyTexas A&M UniversitySearch for more papers by this author and Eric PetersenTexas A&M UniversitySearch for more papers by this authorSession: FD-36: Unsteady Compressible FlowsPublished Online:25 Jun 2012https://doi.org/10.2514/6.2010-926SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byApproximating a far-field blast environment in an advanced blast simulator for explosion resistance testing13 March 2020 | International Journal of Protective Structures, Vol. 11, No. 4Effect of wall heat transfer on shock-tube test temperature at long times9 October 2010 | Shock Waves, Vol. 21, No. 1 What's Popular 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 04 January 2010 - 07 January 2010Orlando, Floridahttps://doi.org/10.2514/6.2010-926 Crossmark TopicsAerodynamicsAerospace SciencesBoundary LayersComputational Fluid DynamicsEquations of Fluid DynamicsFlow RegimesFluid DynamicsFluid MechanicsNumerical AnalysisOblique Shock WaveShock WavesVortex Dynamics KeywordsHigh Enthalpy Shock TunnelTurbulent Boundary LayerComputational Fluid DynamicsAdaptive Mesh RefinementConjugate Heat TransferVortex FilamentsFluid MechanicsAdverse Pressure GradientFlow ConditionsHeat CapacityDigital Topics Aerospace Systems, Operations and Life Cycle