Active separation control for the flying-wing uav using synthetic jet

Engineering

• Boundary Layer 100%
• Separation Control 100%
• Unmanned Aerial Vehicle 50%
• Actuator 50%
• Angle-of-Attack 50%
• Flight Condition 50%
• Flow Characteristic 50%
• Aspect Ratio 50%
• Aerodynamic Characteristic 50%
• Flow Separation 50%