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Design of a laminated composite multi-cel structure subjected to torsion

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Laminate composite multi-cell structures have to support both axial and shear stresses when sustaining variable twist. Thus the properties and design of the laminate may not be the most adequate at all cross-sections to support the torsion imposed on the cells. In this work, the effect of some material and geometric parameters on the optimal mechanical behaviour of a multi-cell composite laminate structure is studied when torsion is present. A particle swarm optimization technique is used to maximize the multi-cell structure torsion constant that can be used to obtain the angle of twist of the composite laminate profile.

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Laminated Composite Optimal Behaviour Particle Swarm Optimization

Citation

BARBOSA, Inês de Carvalho Jerónimo; LOJA, Maria Amélia Ramos – Design of a laminated composite multi-cel structure subjected to torsion. In 29th Congress of the International Council of the Aeronautical Sciences, ICAS. International Council of the Aeronautical Sciences, 2014. ISBN: 3932182804

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International Council of the Aeronautical Sciences

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