Numerical simulation of separated flow control on an airfoil using dual synthetic jets

Engineering

• Actuator 50%
• Aerodynamic Performance 50%
• Airfoil 100%
• Angle-of-Attack 50%
• Characteristic Frequency 50%
• Energetics 50%
• Flow Distribution 50%
• Flow Separate 100%
• Forcing Frequency 50%
• Frequency Coefficient 50%
• Maximum Lift Coefficient 50%
• Momentum Coefficient 100%
• Numerical Computation 50%
• Separated Flow 100%