Numerical Investigation And Validation Of Jet Temperature Effects On Nozzle-Afterbody Drag

Keyphrases

• Nozzle 100%
• Temperature Effect 100%
• Numerical Investigation 100%
• CFD Simulation 100%
• Mach number 100%
• Numerical Validation 100%
• Technical Paper 100%
• Jet Temperature 100%
• Flow Solver 50%
• Flow Condition 50%
• Free Stream 50%
• Turbulence Model 50%
• Airflow 50%
• Accurate Solution 50%
• Specific Heat 50%
• Cold Air 50%
• CFD Approach 50%
• Density-based 50%
• Relative Error 50%
• Convergence Problem 50%
• Algebraic multigrid 50%
• Hot Jet 50%
• Supersonic Flow 50%
• Roe's FDS 50%
• Pressure Ratio 50%
• Multigrid Scheme 50%
• Cold Jet 50%
• Compressible Flow 50%
• Total Pressure 50%
• High Mach number 50%
• Second-order Upwind Scheme 50%
• Static Pressure 50%
• Transonic Flow 50%
• Nozzle Throat 50%
• Drag Coefficient Cd 50%
• Subsonic Flow 50%
• Mente 50%
• Density-based Solver 50%
• Pressure-based Solver 50%

Engineering

• Computational Fluid Dynamics 100%
• Mach Number 50%
• Flow Solver 25%
• Boundary Condition 25%
• Flow Condition 25%
• NASA 25%
• Drag Coefficient 25%
• Air Flow 25%
• Numerical Approach 25%
• Convergence Problem 25%
• Static Pressure 25%
• Constant Specific Heat 25%
• Relative Error 25%
• High Mach Number 25%
• Multigrid Scheme 25%
• Order Upwind Scheme 25%
• Pressure Ratio 25%
• Accurate Solution 25%
• Compressible Flow 25%
• Transonic Flow 25%
• Supersonic Flow 25%
• Subsonic Flow 25%

Material Science

• Computational Fluid Dynamics 100%
• Mach Number 75%
• Density 50%
• Subsonic Flow 25%
• Compressible Flow 25%
• Supersonic Flow 25%
• Transonic Flow 25%