Aerodynamics of biplane and tandem wings at low Reynolds numbers

Engineering

• Angle-of-Attack 100%
• Stall Angle 50%
• Particle Image Velocimetry 50%
• Trailing Edge 50%
• Leading Edge 50%
• Flat Plate 50%
• Aerodynamic Characteristic 50%
• Performance Improvement 50%
• Shear Layer 50%
• Incidence Angle 50%
• Aerodynamic Efficiency 50%
• Aspect Ratio 50%