No AccessNumerical modeling of liquid-liquid bi-propellant droplet/gas reacting flowsYUPAI TANG and M. SCHUMANYUPAI TANGRockwell International Corp., Rocketdyne Div., Canoga Park, CASearch for more papers by this author and M. SCHUMANRockwell International Corp., Rocketdyne Div., Canoga Park, CASearch for more papers by this authorPublished Online:17 Aug 2012https://doi.org/10.2514/6.1992-232SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for references What's Popular 30th Aerospace Sciences Meeting and Exhibit 06 January 1992 - 09 January 1992Reno,NV,U.S.A.https://doi.org/10.2514/6.1992-232 Crossmark TopicsAerodynamicsAerospace SciencesComputational Fluid DynamicsEquations of Fluid DynamicsFlow RegimesFluid DynamicsFluid Flow PropertiesFluid MechanicsNumerical AnalysisOblique Shock WaveReacting FlowShock WavesTurbulenceTurbulence Models KeywordsPropellantNavier Stokes SolverChemically Reacting FlowAxisymmetric FlowRocket InjectorEnergy TransferAstronauticsAeronauticsCombustor DesignChamber PressureDigital Topics Aerospace Systems, Operations and Life Cycle