“…In fact, the influence of the initial conditions on the behaviour of airfoils is one of the main tasks of aeroelastic analysis. The results are referred to as the stability boundary in terms of the initial conditions (Price et al, 1994), boundary for different types of motion , domains of attraction (Levitas et al, 1994;Levitas and Weller, 1995), or simply as parameter maps (Kim and Lee, 1996). Because the cell mapping techniques appear appropriate for the prediction of the boundaries of different types of motion depending on initial conditions, they have been applied in many engineering problems, including the global analysis of bifurcations of the Duffing-van-der-Pol oscillators under both additive and multiplicative random excitations (He et al, 2004), the global analysis of climate predictability (Mu et al, 2004), the optimal control of autonomous dynamical systems (Zufiria and Martinez-Marin, 2003), nonlinear vibrations of a rotor system with bearing clearance ( Karlberg and Aidanpaa, 2003), multiple steady state solutions of a nonlinear system with time-delay (Raghothama and Narayanan, 2002) and the global dynamics of a damped flexible connecting rod (Chen and Chian, 2001).…”