Aerodynamic noise suppression of slats by using a SNGR method

Engineering

• Directivity 100%
• Aerodynamic Noise 100%
• Shear Layer 100%
• Noise Suppression 100%
• Two Dimensional 50%
• Flow Distribution 50%
• Trailing Edge 50%
• Leading Edge 50%
• Noise Source 50%
• Frequency Spectrum 50%
• Acoustic Pressure 50%
• Geometrical Configuration 50%
• Effective Length 50%
• Nonuniform Flow 50%
• Sound Propagation 50%
• Propagation Equation 50%
• Turbulent Velocity 50%
• Pressure Contour 50%