Noise simulations of supersonic hot jets for chevron nozzles

Keyphrases

• Noise Simulation 100%
• Hot Jet 100%
• Chevron Nozzle 100%
• Chevron 75%
• Nozzle 50%
• Noise Prediction 50%
• Interface Conditions 50%
• Nozzle Geometry 50%
• Block Interface 50%
• Mesh Topology 50%
• Operating Conditions 25%
• Space-time Correlation 25%
• Convection Velocity 25%
• Jet Noise 25%
• Noise Source 25%
• Turbulence Intensity 25%
• Two-point 25%
• Simulation Approach 25%
• Acoustic Analogy 25%
• Jet Shear Layer 25%
• Multigrid 25%
• Noise Spectrum 25%
• Mesh Size 25%
• Permeable Surface 25%
• Detached Eddy Simulation 25%
• Tation 25%
• Grid Generation 25%
• Immersed Boundary Method 25%
• Simulation Accuracy 25%
• Dual-time Stepping 25%
• NiTe 25%
• Residual Smoothing 25%
• Broadband Shock-associated Noise 25%
• Structured Mesh 25%

Engineering

• Interface Condition 100%
• Correlation Time 50%
• Computational Fluid Dynamics 50%
• Good Agreement 50%
• Centerline 50%
• Multigrid 50%
• Noise Source 50%
• Shear Layer 50%
• Singularities 50%
• Turbulence Intensity 50%
• Noise Spectra 50%
• Permeable Surface 50%
• Detached Eddy Simulation 50%
• Convection Velocity 50%
• Grid Generation 50%
• Structured Mesh 50%
• Dual Time 50%
• Stepping Approach 50%
• Residual Smoothing 50%
• Mesh Size 50%

Material Science

• Computational Fluid Dynamics 100%