Simulations and measurements of the flow and noise in hot supersonic jets

Keyphrases

• Nozzle 100%
• Numerical Simulation 100%
• Supersonic Jet 100%
• Acoustic Field 100%
• Chevron 100%
• High Performance 50%
• Helium 50%
• Operating Conditions 50%
• Noise Reduction 50%
• Surface Mounting 50%
• Numerical Prediction 50%
• Forward Flight 50%
• Aircraft Engine 50%
• Acoustic Data 50%
• Nozzle Geometry 50%
• Multigrid 50%
• Noise Measurement 50%
• Flow Measurement 50%
• Ffowcs Williams-Hawkings Equation 50%
• Immersed Boundary Method 50%
• Anechoic 50%
• Air Mixture 50%
• Dual-time Stepping 50%
• Body-fitted Grid 50%
• Residual Smoothing 50%
• Hybrid RANS-LES 50%
• Chevron Nozzle 50%
• Non-matching Interfaces 50%
• Multi-block Grid 50%
• Exhaust Jet 50%
• Military Aircraft 50%
• Turbulence Modeling 50%

Engineering

• Jet 100%
• Computer Simulation 66%
• Numerical Prediction 33%
• Aircraft Engine 33%
• Multigrid 33%
• Forward Flight 33%
• Acoustic Far Field 33%
• Acoustic Field 33%
• Measurement Noise 33%
• Dual Time 33%
• Air Mixture 33%
• Residual Smoothing 33%
• Military Aircraft 33%
• Exhaust Gas 33%
• Turbulence Modeling 33%

Physics

• Supersonics 100%
• Acoustics 100%
• Numerical Simulation 66%
• Nozzle Geometry 33%
• Noise Measurement 33%
• Ffowcs Williams-Hawkings Equation 33%
• Aircraft Engine 33%
• Noise Reduction 33%
• Exhaust Gas 33%
• Flow Measurement 33%
• Helium 33%