Mathematical Problems in Engineering / 2012 / Article / Fig 5

Research Article

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

Figure 5

Comparison of LCO response at Mach = 0.825, and .
152123.fig.005a
(a)
152123.fig.005b
(b)

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