Mathematical Problems in Engineering / 2012 / Article / Fig 8

Research Article

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

Figure 8

The LCO amplitude with Mach number (ROM versus full-order model).
152123.fig.008a
(a)
152123.fig.008b
(b)

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