The laminated composite structures can be tailored to design
advanced structures, but the sharp change in the properties of each
layer at the interface between two adjacent layers causes large
inter-laminar shear stresses that may eventually give rise to well
known phenomenon known as delamination. Such detrimental effects
can be mitigated by grading the properties in a continuous manner
across the thickness direction resulting in a new class of
materials known as 'functionally graded materials' (FGMs). This
book presents a non-linear dynamics and vibration analysis on
functionally graded circular and annular plates that are bonded
with piezoelectric actuator layers considering the implications of
thermal effects on piezoelectric behaviour of the coupled
structure.
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