Reduced-Order Modeling for Nonlinear Aeroelasticity with Varying Mach Numbers

Engineering

• Aerodynamic Force 20%
• Aerodynamics 40%
• Aeroelastic Behavior 20%
• Aeroelasticity 100%
• Airfoil 20%
• Computational Fluid Dynamics 20%
• Computational Time 20%
• Flow Characteristic 20%
• Flow Condition 20%
• Flow Parameters 20%
• Frequency Domain 20%
• Gaussian White Noise 20%
• Harmonics 20%
• Limit Cycle 20%
• Mach Number 100%
• Main Flow 20%
• Nonlinear Feature 20%
• Particle Swarm Optimization 20%
• Proper Orthogonal Decomposition 20%
• Recursive 20%
• Reduced Order Model 40%
• Structural Parameter 20%
• Time Domain 20%
• Transonic Flow 40%