2001
DOI: 10.1016/s0266-3538(00)00126-3
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Injection simulations of thick composite parts manufactured by the RTM process

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Cited by 19 publications
(11 citation statements)
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“…A simulation procedure using a quasi-steady formulation based on the Finite Element/ Control Volume Method (FE/CVM) stands out as the most popular, in which the FEM is used to solve for the pressure field which is then used to compute resin flow rates and advance the flow front by filling empty control volumes at the boundary [8][9][10][11][12][13][14]. This approach has an advantage that flow simulation can be carried out without re-meshing the resin-filled domain even though the flow front changes continually.…”
Section: Introductionmentioning
confidence: 99%
“…A simulation procedure using a quasi-steady formulation based on the Finite Element/ Control Volume Method (FE/CVM) stands out as the most popular, in which the FEM is used to solve for the pressure field which is then used to compute resin flow rates and advance the flow front by filling empty control volumes at the boundary [8][9][10][11][12][13][14]. This approach has an advantage that flow simulation can be carried out without re-meshing the resin-filled domain even though the flow front changes continually.…”
Section: Introductionmentioning
confidence: 99%
“…These fluid assumptions also hold true for most resin infusion methods and form the basis for their corresponding numerical models, including RTM simulations. [2][3][4][5][6][7][8] Using finite element (FE) solvers, these models iterate Darcy's law for each FE volume by invoking pre-defined permeability and resin viscosity values and combining them with mass continuity to calculate the local fluid pressure gradient. Non isothermal cases have also been considered 4 where heat transfer and polymerisation exotherm were used to determine the local resin viscosity at finite intervals, which was in turn applied to Darcy's law.…”
Section: Review Of Related Literaturementioning
confidence: 99%
“…Recent developments in structural, load-bearing aircraft components have raised the need for a complete characterisation of the permeability tensor. The diffi culties involved in measuring a three-dimensional (3D) permeability in a single measurement are in general avoided by measuring the in-plane and out-of-plane or transverse permeability K 3 separately, although a few references are available (Ahn et al , 1995;Saouab et al , 2001;Stöven et al , 2003) on measuring the 3D permeability tensor. Stöven et al (2003) performed 3D measurements on NCFs, which are presented in this chapter.…”
Section: © Woodhead Publishing Limited 2011mentioning
confidence: 99%