Advances in Material Forming
DOI: 10.1007/978-2-287-72143-4_5
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Composites Forming

Abstract: The strong development of composite materials in particular in aeronautics leads to a demand for knowledge and simulation codes concerning composites forming. The mini-symposia developed on this theme within the ESAFORM conference are a privileged framework for the researchers in this field to communicate and to exchange ideas. This paper gives a progress report on the advancements achieved during these ten last years and on the research prospects in the various fields of composite material forming.

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Cited by 15 publications
(11 citation statements)
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“…Characterisation of the deformability of reinforcements via testing and/or meso-modelling of deformation provides input for macro-modelling of the drapability, used for optimisation of the preform architecture and process conditions. High cost of the materials used make adequate simulation tools essential for industry and drive the wide research efforts worldwide [2][3][4][5].…”
Section: Introductionmentioning
confidence: 99%
“…Characterisation of the deformability of reinforcements via testing and/or meso-modelling of deformation provides input for macro-modelling of the drapability, used for optimisation of the preform architecture and process conditions. High cost of the materials used make adequate simulation tools essential for industry and drive the wide research efforts worldwide [2][3][4][5].…”
Section: Introductionmentioning
confidence: 99%
“…wrinkling, tearing) determine the product quality. Simulation tools that link product quality to material, mold and process parameters are being developed to support design and process optimization [1][2][3]. The prediction of local deformations is an essential task within this objective.…”
Section: Introductionmentioning
confidence: 99%
“…While most of the effort is focused on developing constitutive models to represent the behaviour of the dry fabric during draping [3], it has been evidenced in recent studies that the forming cannot be considered adiabatic: when the laminate contacts the tool, its temperature rapidly decreases which can lead to local rigidification and formation of wrinkles. The thermomechanical models proposed thus far are either isothermal [4] or assume an homogeneous temperature field in the blank at the beginning of the forming step [5], which is complex to achieve in practice given the low conductivity of the polymers.…”
Section: Introductionmentioning
confidence: 99%