Nozzle wall modeling in unstructured large eddy simulations for hot supersonic jet predictions

Keyphrases

• Large Eddy Simulation 100%
• Nozzle 100%
• Supersonic Jet 100%
• Wall Modeling 100%
• Turbulence Model 50%
• Inlet Conditions 50%
• Dual-stream 50%
• High-frequency Noise 25%
• Laminar-turbulent Transition 25%
• Boundary Layer 25%
• Laminar Boundary Layer 25%
• Flow Modeling 25%
• Near-wall Region 25%
• Velocity Fluctuation 25%
• Noise Measurement 25%
• Shear Layer 25%
• Nozzle Exit 25%
• Numerical Prediction 25%
• Jet Plume 25%
• Peak Velocity 25%
• Noise Source 25%
• Turbulent Shear Layer 25%
• Converging-diverging 25%
• Far-field Noise 25%
• Radiated Noise 25%
• Dual-stream Jet 25%
• Mesh Refinement 25%
• Mesh Resolution 25%
• Bypass Ratio 25%
• Circular Nozzle 25%
• External Flow Field 25%
• Inflow Turbulence 25%
• Internally Mixed 25%
• Refined Simulation 25%
• Synthetic Inflow Turbulence 25%
• Mesh Adaptation 25%

Engineering

• Shear Layer 100%
• Boundary Layer 50%
• NASA 50%
• Good Agreement 50%
• Laminar Boundary Layer 50%
• Measurement Noise 50%
• Velocity Fluctuation 50%
• Numerical Prediction 50%
• Frequency Noise 50%
• Nozzle Exit 50%
• Noise Source 50%
• Noise Field 50%
• Radiated Noise 50%
• External Flow 50%
• Circular Nozzle 50%
• Peak Velocity 50%
• Mesh Refinement 50%
• Bypass Ratio 50%
• Flow Distribution 50%