Laminate composites can be used quite naturally in automotive, marine, aviation and
other engineering branches. Determination of buckling load capacity under in-plane composite
loads of composite plates is very important for the design of composite structures. In this thesis,
Differential Evolution (DE) and Simulated Annealing (SA) are utilized for optimal stacking
sequence of a laminated composite plate, which is simply supported on four edges and is
subjected to biaxial in-plane compressive loads. The optimization problem parameters are
defined as
(i) Objective function: critical buck ...Daha fazlası
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