Structural Health Monitoring with Piezoelectric Wafer Active Sensors

In this chapter, we will analyze plate vibration. After reviewing the general plate equations, we will consider two situations separately: (a) axial vibration of plates; and (b) flexural vibration of plates.
Because the plate surface is free, the z-direction stress is assumed to be zero ( ? zz = 0). Also zero are assumed to be the surface shear stresses ? yz = 0 and ? zx = 0. Hence, the 3-D elasticity relations given in Appendix B reduce to
In our analysis, we are only interested in the strains ? xx, ? yy, ? xy. Solution of Eq. (1) yields
Axial vibrations are related to extension/compression motion in the plate, i.e., the motion is in-plane polarized.
Assume in-plane displacements u( x, y, t) and v( x, y, t) which are uniform across the plate thickness. The strains of interest are
The strains are constant across the plate thickness. Substitution of Eq. (3) into Eq. (2) yields
Note that the stresses are also constant across the plate thickness. Integration of stresses across the plate thickness gives the stress resultants (forces per unit width) N x, N y, and N xy shown in Fig. 4.1, i.e.,
Newton...