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Book ChapterDOI

Multilevel Optimization Procedure of Composite Structure

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TLDR
In this paper, a multilevel optimization procedure for minimum weight design of composite structures is presented, where the optimization process is divided into two levels: system level and component level.
Abstract
We present a multilevel optimization procedure for minimum weight design of composite structures. The optimization process is divided into two levels: system level and component level. In system level the thicknesses of laminated composite plates represent the design variables. The well-known optimality criterion method based on the Kuhn-Tucker condition is used to modify the design variables. The detail design of laminated plates, i.e. to determine the optimal ply thicknesses, is handled in component level In component level, keeping the thickness of laminated composite plates and the nodal displacements invariant, the ply thicknesses are adjusted according to the strain energy possessed by each ply. As an illustrative example, a cantilever composite beam, which is subjected to several load conditions and multiple constraints, is studied. All the five examples given in this chapter present very satisfactory results. In general the optimal design can be obtained after 3–5 iterations.

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Citations
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Journal ArticleDOI

Design of composite laminates by a Monte Carlo method

TL;DR: In this article, a Monte Carlo procedure was developed for optimizing symmetric fiber reinforced composite laminates such that the weight is minimum and the Tsai-Wu strength failure criterion is satisfied in each ply.
Journal ArticleDOI

Design of laminated composite structures for optimum fiber direction and layer thickness, using optimality criteria

TL;DR: In this paper, two optimality criteria are presented for optimum design of composite laminates using finite element method, namely, thickness of the layers and fiber orientation angles in each finite element are considered as the design variables.
Journal ArticleDOI

Design of Composite Laminates for Strength, Weight, and Manufacturability

TL;DR: In this article, a procedure is presented for determining the layups of unidirectional fiber reinforced composite plates (with or without cutouts) subjected to multiple in-plane and out-of-plane loadsets, such that the plate satisfies the Tsai-Wu Quadratic Strength Failure criterion, is of low weight, and has a layup which is easy to manufacture.
Journal ArticleDOI

Optimization of laminated composite structures using a bilevel strategy

TL;DR: In this article, the optimal design of laminated composite structures is investigated using a combination of sensitivity analysis combined with optimality criteria and mathematical programming, and the adequacy of the solution is assured by constraints limiting stresses and displacements.
Journal ArticleDOI

Optimum design based on reliability for composite laminate layup

TL;DR: In this article, the authors presented a method for obtaining optimum design based on reliability of composite structures, which is subject to main structural system reliability constraint and some secondary constraints (i.e. minimum ratio of thickness, balance and symmetry).
References
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Book ChapterDOI

Introduction To Composite Materials

TL;DR: The combination of materials to form a new material system with enhanced material properties is a well documented historical fact as discussed by the authors, which is why many artisans from the Mediterranean and Far East used a form of composite technology in molding art works which were fabricated by layering cut paper in various sizes for producing desired shapes and contours.
Book

Introduction to composite materials

TL;DR: In this paper, the authors present a reference record created on 2005-11-18, modified on 2016-08-08 and used for Laminage Reference Record created on 2006-11/18.
Journal ArticleDOI

Optimum Design of Composite Structures with Stress and Displacement Constraints

TL;DR: In this paper, a recurrence relation based on an optimality criterion is used to modify the design variables during the iterative procedure, taking into account the effects of multiple displacement constraints, multiple loading conditions, and variable allowable stresses.
Proceedings ArticleDOI

A multilevel method for structural synthesis

TL;DR: In this paper, a multilevel method for structural synthesis based on finite element modeling at both the system and the substructure level is presented, where the design is described using basis vectors generated via substructure design modification.
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