Abstract:
This paper presents an analytical solution for free
vibration response of orthotropic laminated plate with
piezoelectric layers based on a new procedure that is
m simpler than those presented by Pagano and Fan. In
the analysis, the 3-D piezoelectric theory is employed to
develop a new concise formula for composite laminates.
The natural frequencies and the corresponding mode
distributions have been computed for three aspects of
thickness/span of a five-layer piezoelectric laminated
plate with simply supported and grounded boundaries
under cylindrical bending.