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What is Buckling Optimization of Composite Shells about?

This document discusses using topology optimization to maximize the buckling load factor of laminated composite shell structures. It presents an approach called Discrete Material Optimization (DMO) that allows choosing the best material and fiber orientation for each layer of a composite structure to improve its buckling performance. Examples applying DMO to optimize laminated plates and a simplified wind turbine blade shell model are given to illustrate its potential for solving the combinatorial problem o

Author

ali_biscoeat

Language

EN