No AccessNumerical Investigation of Transcritical Turbulent Channel FlowAlexander Doehring, Steffen Schmidt and Nikolaus AdamsAlexander DoehringTechnical University of MunichSearch for more papers by this author, Steffen SchmidtTechnical University of MunichSearch for more papers by this author and Nikolaus AdamsTechnical University of MunichSearch for more papers by this authorAIAA 2018-4768Session: German SFBTRR-40 III - Combustion and CoolingPublished Online:8 Jul 2018https://doi.org/10.2514/6.2018-4768SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byLarge-eddy simulation of turbulent channel flow at transcritical statesInternational Journal of Heat and Fluid Flow, Vol. 89Assessment of RANS Turbulence Models for Straight Cooling Ducts: Secondary Flow and Strong Property Variation Effects27 October 2020Towards Direct Numerical Simulations of Shock-Turbulence Interaction in Real Gas Flows on GPUs: Initial Validation9 July 2020Related articlesCorrection: Numerical Investigation of Transcritical Turbulent Channel Flow24 Jul 2018AIAA Propulsion and Energy Forum What's Popular 2018 Joint Propulsion Conference July 9-11, 2018Cincinnati, Ohiohttps://doi.org/10.2514/6.2018-4768 CrossmarkInformationCopyright © 2018 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. TopicsAerodynamicsBoundary LayersComputational Fluid DynamicsConservation of Momentum EquationsEquations of Fluid DynamicsFinite Volume MethodFlow RegimesFluid DynamicsFluid Flow PropertiesHeat TransferNumerical AnalysisNumerical Heat TransferNumerical InterpolationThermophysics and Heat TransferVortex Dynamics KeywordsIncompressible FlowDirect Numerical SimulationHeat Transfer CoefficientsThermodynamic PropertiesThermal DiffusivityNavier Stokes EquationsLiquid Rocket EngineRegenerative CoolingVelocity ProfilesBoundary Layer ThicknessPDF Topics Liquid Propulsion