Following laminated composite plates and beams, tapered laminated structure
s, which are formed by dropping off some of the plies at discrete positions
over the laminate, have received much attention from researchers because o
f their structural tailoring capabilities, damage tolerance, and their pote
ntial for creating significant weight savings in engineering applications.
A review of recent developments in the analysis of tapered laminated compos
ite structures with an emphasis on interlaminar stress analysis, delaminati
on analysis and parametric study is presented. A discussion of Various appr
oaches to modelling and analysis of interlaminar response of tapered compos
ites using finite elements and non-finite elements is given. Displacement-b
ased finite elements and hybrid finite elements that are commonly used are
also reviewed. A review of various studies on delamination failure mechanis
ms as a result of drop-off plies in the tapered composites is given next, w
hich mainly encompasses a stress-strength approach and a fracture-mechanics
approach. Lastly, a variety of methods that are being used in the parametr
ic studies regarding the structural integrity is presented. Overall remarks
drawn from the reviewed works are given in the final section of the paper.
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