Research Article

Higher Period Stochastic Bifurcation of Nonlinear Airfoil Fluid-Structure Interaction

Figure 15

Response surface of the pitch angle 𝛼 at 𝜏 = 2 0 0 0 as function of the random initial condition 𝛼 0 .
394387.fig.0015a
(a)
394387.fig.0015b
(b)
394387.fig.0015c
(c)
394387.fig.0015d
(d)