Internal accoustic excitation to enhance the airfoil performance at high reynolds number

Engineering

• Airfoil 100%
• Flow Separation 100%
• Lifting Surface 100%
• High Reynolds Number 100%
• Angle-of-Attack 66%
• Open Circuit 33%
• Excitation Frequency 33%
• Energy Input 33%
• Boundary Layer Separation 33%
• Fluid Momentum 33%
• Stall Angle 33%
• Pressure Flow 33%
• Shedding Frequency 33%
• Acoustic Vibration 33%
• Leading Edge 33%
• Strouhal Number 33%
• Air Flow 33%
• Jet 33%
• Wind Tunnels 33%

Keyphrases

• Accoustic 100%
• Adverse Pressure 33%
• μ-open Set 33%
• Top Surface 33%
• Open Jet 33%
• Stall Angle of Attack 33%

Physics

• Strouhal Number 50%