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• W4247972812 abstract "This chapter contains sections titled: PDF/FDF-Methods for the Prediction of Supersonic Turbulent Combustion Introduction Methods for Turbulent Reacting Flow Calculations Basic Methods Hybrid PDF/FDF-Methods Some Deficiencies of Existing Hybrid PDF-Methods The Transport Problem The Mixing Problem The Energy Problem New Theoretical Concepts The Transport Problem The Mixing Problem The Energy Problem The Use of PDF Combustion Codes The Current Use of PDF/FDF-Methods New Developments Common Activities to Develop a New Combustion Code Prospects for Further Developments The Current and Future Use of Computational Methods Some Challenges Design and Testing of Gasdynamically Optimized Fuel Injectors for the Piloting of Supersonic Flames with Low Losses Introduction Experimental Setup Model SCRamjet Combustor Preheater Combustion Chamber Injectors Investigation Tools Shadowgraph Method Rayleigh Scattering Raman Scattering OH-LIF Measurements Self-Fluorescence Measurements (Chemiluminescence) Numerical Modelling Numerical Simulation with the CFD-Code Fluent 5.5 Special Features of the Modelling of the Supersonic Combustion Reducing the Number of Species Reaction Mapping by Using of the Polynomials Validation of the Modelling Approach with Polynomials Two Stage Injector Theoretical Considerations Shock Stabilization Combustion Conclusions Hypersonic Propulsion Systems: Design, Dual-Mode Combustion and Systems Off-Design Simulation Combustion Stability of a Dual-Mode Scramjet Configuration with Strut Injector Introduction Experimental Setup Results and Discussion Conclusions Hypersonic Highly Integrated Propulsion Systems Design and Off-Design Simulation Introduction Reference Propulsion System for the TSTO Concept Engine Integration Core Engine Numerical Engine Simulation Thrust Vectoring Real Time Flight Simulation Conclusion Experimental Investigation about External Compression of Highly Integrated Airbreathing Propulsion Systems Introduction Focus on the Problem Preliminary Measurements Experimental Facility Wind Tunnel Models and Instrumentation Model 1 Model 2 Model 3 Numerical Model Measurements and Results Determination of the Boundary-Conditions Measurements in the Field of Shock Boundary Layer Interaction Conclusion and Outlook Experimental and Numerical Investigation of Lobed Strut Injectors for Supersonic Combustion Introduction Experimental Setup and Measurement Techniques Governing Equations and Numerical Simulation Multigrid Convergence Acceleration Strut Design and Performance Parameters Supersonic Mixing Supersonic Combustion Investigation of Different Lobed Strut Injectors Conclusions Experimental Studies of Viscous Interaction Effects in Hypersonic Inlets and Nozzle Flow Fields Introduction Experimental Techniques Facility and Flow Diagnostics Wind Tunnel Models Inlet Studies Nozzle Studies Conclusion Intake Flows in Airbreathing Engines for Supersonic and Hypersonic Transport Introduction Physical Model Numerical Method Results Turbulent 2D Supersonic Intake Flows with Internal Compression Laminar 3D Hypersonic Corner Flows Turbulent 3D Hypersonic Flows through Symmetric/Asymmetric Double-Fin Configurations Laminar 2D Shock Interactions in Hypersonic Flows with Chemical Non-Equilibrium Conclusions" @default.
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• W4247972812 date "2005-05-09" @default.
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• W4247972812 title "Propulsion" @default.
• W4247972812 doi "https://doi.org/10.1002/3527605711.ch5" @default.
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