Multipulse Heteroclinic Orbits and Chaotic Dynamics of the Laminated Composite Piezoelectric Rectangular Plate

Figure 7

The bifurcation diagram is obtained for the damping coefficients 𝜇₂= 0.06~0.6, 𝑓₂=55.1, and 𝜇₁=0.1; (a) the bifurcation diagram on the plane (𝑥₁,𝜇₂); (b) the bifurcation diagram on the plane (𝑥₃,𝜇₂).

(a)

(b)