It is feasible to design laminated composites with negative Poisson's ratio
. Although the minimum value of negative Poisson's ratio design can be done
via numerical approach, it is possible to use the analytical method in thi
s paper to perform the following tasks: (a) evaluate the approximated ply o
rientation angles to obtain maximum transverse strain epsilon(gamma), (b) d
etermine the necessary conditions of design negative Poisson's ratio,and (c
) investigate the influence of laminae properties on the Poisson's ratio of
a composite laminate.
In this study, it is also found that, in general, the ply orientations for
obtaining maximum transverse strain, epsilon(gamma), in a composite laminat
e are close to [70 degrees/20 degrees](S).