No AccessEvaluating the Correlations for Supersonic Spray CombustionFoluso LadeindeFoluso LadeindeStony Brook UniversitySearch for more papers by this authorAIAA 2019-0125Session: Numerical Analysis of Scramjet EnginesPublished Online:6 Jan 2019https://doi.org/10.2514/6.2019-0125SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byProgress in Supersonic Spray Combustion ModelingFoluso Ladeinde5 January 2020A Theory for Momentum, Energy, and Mass Transport in Supersonic Spray CombustionFoluso Ladeinde16 August 2019 What's Popular AIAA Scitech 2019 Forum 7-11 January 2019San Diego, Californiahttps://doi.org/10.2514/6.2019-0125 CrossmarkInformationCopyright © 2019 by Foluso Ladeinde. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsAerodynamicsAerospace SciencesCFD CodesComputational Fluid DynamicsEnthalpyEquations of Fluid DynamicsFlow RegimesFluid DynamicsFluid Flow PropertiesHeat TransferThermodynamic PropertiesThermodynamicsThermophysics and Heat Transfer KeywordsDrag CoefficientHeat Transfer CoefficientsCFD CodesConservation of MassShear StressSupersonic CombustionConvective FlowProbability DistributionEnthalpy of VaporizationCritical TemperatureDigital Topics High-Speed Air-Breathing Propulsion