Abstract
A multilayered plate element combined with a micromechanical analysis of fibrous composite materials is incorporated in the energy-based optimization of laminated structures. The internal stresses or eigenstresses, promoted here by manufacturing processes, are introduced as control parameters to provide for a minimum of various objective functionals. The optimal values of the fiber eigenstresses are found employing the combinatorial optimization technique known as a simulated annealing. Results are presented for the B/A1 composite system.
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