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

Figure 6

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

(a)

(b)