Hybrid Aero-Acoustics Prediction Method Coupled with RANS/LES Model and LEE Equation

Engineering

• Sound Source 100%
• Turbulent Velocity 100%
• Acoustic Propagation 66%
• Sound Pressure Level 66%
• Aerodynamic Noise 66%
• Hybrid Method 66%
• Experimental Result 33%
• Flow Distribution 33%
• Euler Equation 33%
• Boundary Condition 33%
• Sound Pressure 33%
• Acoustic Field 33%
• Peak Value 33%
• Frequency Spectrum 33%
• Source Term 33%
• Discretization 33%
• Linearized Euler Equation 33%
• Monitoring Point 33%
• Sound Propagation 33%
• Propagation Equation 33%
• Field Boundary 33%