Experimental investigation of lift enhancement and drag reduction of discrete co-flow jet rotor airfoil

Engineering

• Rotors 100%
• Airfoil 100%
• Experimental Investigation 100%
• Drag Reduction 100%
• Maximum Lift Coefficient 37%
• Angle-of-Attack 25%
• Stall Angle 25%
• Length Unit 25%
• Tunnel 12%
• Rotor Blade 12%
• Optimal Performance 12%
• Performance Improvement 12%
• Drag Coefficient 12%
• Lift to Drag Ratio 12%
• Fundamental Problem 12%
• Helicopter Rotors 12%