Influence of Pitch, Twist, and Taper on a Blade's Performance Loss Due to Roughness

Engineering

• Performance Degradation 100%
• Pitch Angle 100%
• Rotors 100%
• Performance Loss 100%
• Geometric Parameter 100%
• Test Data 50%
• Angle-of-Attack 50%
• Parametric Study 50%
• Edge Roughness 50%
• Roughness Effect 50%
• Surface Condition 50%
• Airfoil Geometry 50%
• Airfoil 50%
• Leading Edge 50%
• Tunnel 50%