Iris Publishers - Global Journal of Engineering Sciences (GJES)
Effect of Boundary Conditions on Buckling Load for
Laminated Composite Plates
Authorized
by Osama Mohammed Elmardi Suleiman
It
is observed that, for all cases the buckling load increases with the mode
number but at different rates depending on whether the plate is simply
supported, clamped or clamped – simply supported. The buckling load is a
minimum when the plate is simply supported and a maximum when the plate is
clamped. Because of the rigidity of clamped boundary condition, the buckling
load is higher than in simply supported boundary condition. It is also observed
that as the mode number increases, the plate needs additional support.
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