Hybrid computational aeroacoustics approach based on the synthetic turbulence model in Eulerian description

Engineering

• Acoustic Perturbation 100%
• Airfoil 50%
• Boundary Condition 50%
• Computational Cost 50%
• Convective 50%
• Discretization 100%
• Good Agreement 50%
• Mesh Particle 50%
• Modified Model 50%
• Noise Field 50%
• Perturbation Equation 100%
• Reference Data 50%
• Reynolds-Averaged Navier-Stokes 50%
• Sound Source 50%
• Spatial Correlation 50%
• Turbulent Velocity 50%
• Two Dimensional 50%