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Composite finite element model

In Figure 5.23 the finite element model predictions based on with constraint and unconstrained boundary conditions for the modulus of a glass/epoxy resin composite for various filler volume fractions are shown. [Pg.187]

Nassehi, V., Kinsella, M. and Mascia, 1.., 1993b. Finite element modelling of the stress distribution in polymer composites with coated fibre interlayers. J. Compos. Mater. 27, 195-214. [Pg.189]

Daoust, J., Vu-Khanh, T., Ahlstrom, C. and Gerard, J.F. (1993). A finite element model of the fragmentation test for the case of a coated fiber. Composites Sci. Technol. 48, 143-149. [Pg.164]

A single screw extruder was used to fabricate the filaments from the composite. The glass transition of the composite was found to be 126°C, which is higher than that of pure ABS material. In addition, the melt flow behavior was extensively studied by setting up a finite element model (79). [Pg.236]

Figure 4. Composite Shell Finite Element Model... Figure 4. Composite Shell Finite Element Model...
Finite element modelling of the effects of a 14% volume fraction of glass fibre with an aspect ratio of 30 (Fig. 4.29b), used fibre orientations that fitted a maximum entropy distribution. It predicted that the longitudinal Young s modulus increased non-linearly with cos B, and that constant strain conditions applied for averaging the properties of the unidirectional composite. [Pg.130]

Matthews FL, Davies GAO, Hitchings D, Soutis C. Finite element modelling of composite materials and structures. Woodhead Publishing Ltd 2000. [Pg.17]

Bedogni E, Ivanov DS, Lomov SV, Pirondi A, Vettori M, Verpoest I. Creating finite element model of 3D woven fabrics and composites semi-authomated solution of interpenetration problem. In 15th European conference on composite materials (ECCM-15) 2012. Venice, p. electronic edition, s.p. [Pg.50]

D Amato E. Finite element modelling of textile composites. Compos Stmct 2002 54 467-75. [Pg.50]

Mahadik Y, Hallett SR. Finite element modelling of tow geometry in 3D woven fabrics. Composites Part A 2010 41 1192—200. [Pg.51]

A future trend in composite bolted joint design is the use of more advanced continuum damage mechanics approaches to model joint failure, so that non-linear shear behaviour and gradual stiffness degradation can be implemented. An important element of joint failure is delamination, and many efforts are being undertaken to implement delamination in finite element models. However, for bolted joints analysis this poses many problems due to the large number of delamination interfaces in thick laminates. [Pg.328]

Kotzakolios T, Vlachos DE, Kostopoulis V. Blast response of metal composite laminate fuselage structures using finite element modelling. Compos Struct 2011 93 665—81. [Pg.389]

Finite element modelling of composite materials and structures... [Pg.534]

Bogetti, T. A., Wang, T., Van Landringham, M. R., Eduljee, R. E, and Gillespie, J. W. J. 1999. Characterization of nanoscale property variations in polymer composite systems Part 2—finite element modeling. Composites Part A 30, 85-94. [Pg.383]

Tosti et al. [22] compared a thin-walled dense tube Pd membrane and composite Pd-ceramic tube membranes. They developed a finite elemental model for membrane reactors. Table 6.1 shows the WGS reaction conversion values calculated for the dense and the composite membrane reactors both by taking into account the wall effects ( WE case) resistance and by neglecting such a resistance ( no WE case). The main result is that by increasing the temperature the reactiOTi conversion increases. Table 6.2 shows in co-current mode. Both the membranes show similar activities. [Pg.147]

In order to verify some of the predictive capabilities of the finite element model described in the previous sections, the transverse creep response of a IM7/5260 composite investigated in a earlier study [8] was used as a benchmark case. Two separate load histories were considered (1) transverse creep and recovery of a [90]i6 specimen under isothermal conditions, and (2) transverse creep of a [90]i6 specimen subjected to cyclic thermomechanical loading for extended periods of time. [Pg.361]

Tserpes, K. 1. Papanikos, P. (2005). Finite Element Modeling of Single-Walled Carbon Nanotubes. Composites PartB, 36, 468-477. [Pg.263]

Finite element models based on ZrB - 30 vol % SiC composites containing idealized round SiC particles, predicted compressive residual stresses in the dispersed SiC particles while the ZrBa matrix immediatelv surrounding each particle was in tension. Previously an Eshelby analysis shown in equation 6 , had been used to predict radial compressive stresses of as high as 2.1 GPa within the ZrB2 matrix and tangential tensile stresses of 4.2 GPa at the ZrB2-SiC boundaries. ... [Pg.70]

The mechanism of stress transfer from the plastic matrix to the wood particles and vice versa was investigated by Sretenovic et al. [68]. They measured the strain distribution around the particle using electronic speckle pattern interferometry (ESPI). They also conducted an analytical analysis and finite element modelling of strain and stress distribution in the wood plastic composite. [Pg.394]


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