Active flutter suppression of a two-dimensional airfoil section using μ synthesis

Engineering

• Airfoil Section 100%
• Computer Simulation 50%
• Control Loop 50%
• Control Surfaces 50%
• Critical Flutter Speed 50%
• Delay Time 50%
• Flow Speed 50%
• Modeling Error 50%
• Two Dimensional 100%
• Ultrasonics 100%
• Wind Tunnel Test 50%

Physics

• Airfoil Profiles 100%
• Control Surfaces 50%
• Ultrasonics 100%
• Wind Tunnel Test 50%