Influence of aspect ratio on dynamic stall of a finite wing

Keyphrases

• Airfoil 20%
• Angle of Attack 20%
• Aspect Ratio 100%
• Damping Characteristics 20%
• Dynamic Stall 100%
• Dynamic Stall Vortex 20%
• Experimental Performance 40%
• Finite Wing 100%
• Flow Components 20%
• Flow Separation 20%
• High Angle of Attack 20%
• NACA0012 Airfoil 20%
• Performance Data 40%
• Pitch Damping 20%
• Pitch Maneuver 20%
• Pitching Oscillation 20%
• Reduced Frequency 20%
• Reynolds number 20%
• Separation Process 20%
• Spanwise Flow 20%
• Three-dimensional (3D) 20%
• Unsteady Loads 20%
• Unsteady Separation 40%
• Velocity Field 20%
• Velocity Field Measurement 20%
• Velocity Measurement 20%
• Vortex 20%
• Wing Model 20%
• Wingtip 20%

Engineering

• Airfoil 40%
• Angle-of-Attack 40%
• Aspect Ratio 100%
• Field Measurement 20%
• Flow Separation 20%
• Inboard Wing 20%
• Leading Edge 20%
• Led Process 20%
• Performance Data 40%
• Reynolds' Number 20%
• Velocity Component 20%
• Velocity Field 40%
• Vortex 40%