Unstable unsteady aerodynamic modeling based on least squares support vector machines with general excitation

Engineering

• Least Square 100%
• Support Vector Machine 100%
• Aerodynamic Modeling 100%
• Hysteresis Loop 66%
• Mach Number 33%
• Predicted Result 33%
• Computational Fluid Dynamics 33%
• Airfoil 33%
• Wind Tunnel Test 33%
• Aerodynamic Force 33%
• Test Data 33%
• Lift Coefficient 33%
• Drag Coefficient 33%
• Forced Vibration 33%
• Pitching Moment Coefficient 33%
• Nonlinear System Identification 33%