Active control of shock/boundary layer interaction in transonic flow over airfoils

Keyphrases

• Active Control 100%
• Active Flow Control 50%
• Aerodynamic Force 50%
• Aerodynamic Moment 50%
• Aerospace Vehicle 50%
• Airfoil 100%
• Airfoil Surface 50%
• Amplitude Frequency 50%
• Angle of Attack 50%
• Free Stream 50%
• Jet Actuator 50%
• Mach number 50%
• Numerical Simulation 50%
• Pitching Moment Coefficient 50%
• Reynolds number 50%
• Shock Wave Boundary Layer Interaction 100%
• Shock Waves 50%
• Transonic Flow 100%
• Vehicle Attitude Control 50%

Engineering

• Active Control 100%
• Aerodynamic Force 50%
• Aerospace Vehicle 50%
• Airfoil 100%
• Airfoil Surface 50%
• Angle-of-Attack 50%
• Attitude Control 50%
• Boundary Layer 100%
• Jet 50%
• Jet Actuator 50%
• Layer Interaction 100%
• Mach Number 50%
• Oscillatory 100%
• Pitching Moment Coefficient 50%
• Reynolds' Number 50%
• Transonic Flow 100%