Support-Vector-Machine-Based Reduced-Order Model for Limit Cycle Oscillation Prediction of Nonlinear Aeroelastic System

<table>Comparison of aerodynamic response at Mach = 0.825.</table>

Mathematical Problems in Engineering

Figure 4: Support-Vector-Machine-Based Reduced-Order Model for Limit Cycle Oscillation Prediction of Nonlinear Aeroelastic System 