Efficient method for limit cycle flutter analysis by nonlinear aerodynamic reduced-order models

Engineering

• Aerodynamics 100%
• Limit Cycle 100%
• Reduced Order Model 100%
• Computational Fluid Dynamics 40%
• Nonlinearity 40%
• Input Signal 40%
• Aerodynamic Model 40%
• Radial Basis Function 20%
• Design Method 20%
• Network Model 20%
• Angle-of-Attack 20%
• Computational Cost 20%
• Structural Response 20%
• Dynamic Pressure 20%
• Dynamic Method 20%
• Computational Efficiency 20%
• Structural Model 20%
• System Response 20%
• Transonic Flow 20%
• Wave Motion 20%
• Separated Flow 20%
• Aerodynamic Analysis 20%