Academic literature on the topic '3D WOVEN COMPOSITES'

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Journal articles on the topic "3D WOVEN COMPOSITES"

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Siddique, Amna, Baozhong Sun, and Bohong Gu. "Structural influences of two-dimensional and three-dimensional carbon/epoxy composites on mode I fracture toughness behaviors with rate effects on damage evolution." Journal of Industrial Textiles 50, no. 1 (December 22, 2018): 23–45. http://dx.doi.org/10.1177/1528083718819871.

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This paper reports the mode I interlaminar fracture toughness and fracture mechanisms of two-dimensional (2D) plain woven composite and three-dimensional (3D) angle-interlock woven composite. The fracture toughness behaviors were tested with double cantilever beam method at the different loading rates from 0.5 to 100 mm/min. Critical strain energy release rate was calculated to compare the difference between the 2D and the 3D woven composites. The fractographs were photographed with scanned electronic microscopy and optical microscopy to show the fracture morphologies. We found that the 3D angle-interlock woven composite has high fracture toughness than that of 2D woven composite. The binder yarns resist the crack initiation and propagation to increase the fracture toughness. While the lower in-plane stiffness of the 3D woven composites should be considered fully for designing the 3D woven composites.
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Hamada, Hiroyuki, Akihiro Fujita, Zenichiro Maekawa, and Masaya Kotaki. "Bending Properties of 3D Glass Woven Fabric Reinforced Composites." Advanced Composites Letters 2, no. 4 (July 1993): 096369359300200. http://dx.doi.org/10.1177/096369359300200406.

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3D glass woven fabric (PARABEAM) reinforced composites are of particular interest to composite industry, because light weight large scale composite structures can be fabricated. Bending properties of hybrid composites with 3D fabric and chopped strand mat were possible to be estimated by using theory of composite beam. The relations between thickness, weight and bending properties of the 3D composites could be drawn for designing composite structure.
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Fan, Wei, Dan-dan Li, Jia-lu Li, Juan-zi Li, Lin-jia Yuan, Li-li Xue, Run-jun Sun, and Jia-guang Meng. "Electromagnetic properties of three-dimensional woven carbon fiber fabric/epoxy composite." Textile Research Journal 88, no. 20 (July 31, 2017): 2353–61. http://dx.doi.org/10.1177/0040517517723022.

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To investigate the reinforcement architectures effect on the electromagnetic wave properties of carbon fiber reinforced polymer composites, three-dimensional (3D) interlock woven fabric/epoxy composites, 3D interlock woven fabric with stuffer warp/epoxy composites, and 3D orthogonal woven fabric/epoxy composites were studied by the free-space measurement system. The results showed that the three types of 3D woven carbon fiber fabric/epoxy composites had a slight difference in electromagnetic wave properties and the absorption was their dominant radar absorption mechanism. The electromagnetic wave absorption properties of the three types of composites were more than 90% (below −10 dB) over the 11.2–18 GHz bandwidth, and more than 60% (below −4 dB) over the 8–12 GHz bandwidth. Compared with unidirectional carbon fiber reinforced plastics, the three kinds of 3D woven carbon fiber fabric/epoxy composites exhibited better electromagnetic wave absorption properties over a broadband frequency range of 8–18 GHz. Therefore, the three kinds of 3D woven composite are expected to be used as radar absorption structures due to their excellent mechanical properties and outstanding absorption capacity. The total electromagnetic interference shielding effectiveness of the three types of 3D carbon fiber woven composites are all larger than 46 dB over the 8–12 GHz bandwidth, which is evidence that the three types of 3D carbon fiber woven composites can be used as excellent shielding materials for electromagnetic interference.
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Tripathi, Lekhani, and B. K. Behera. "Review: 3D woven honeycomb composites." Journal of Materials Science 56, no. 28 (July 9, 2021): 15609–52. http://dx.doi.org/10.1007/s10853-021-06302-5.

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Hu, Qiaole, Hafeezullah Memon, Yiping Qiu, Wanshuang Liu, and Yi Wei. "A Comprehensive Study on the Mechanical Properties of Different 3D Woven Carbon Fiber-Epoxy Composites." Materials 13, no. 12 (June 18, 2020): 2765. http://dx.doi.org/10.3390/ma13122765.

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In this work, the tensile, compressive, and flexural properties of three types of 3D woven composites were studied in three directions. To make an accurate comparison, three 3D woven composites are made to have the same fiber volume content by controlling the weaving parameters of 3D fabric. The results show that the 3D orthogonal woven composite (3DOWC) has better overall mechanical properties than those of the 3D shallow straight-joint woven composite (3DSSWC) and 3D shallow bend-joint woven composite (3DSBWC) in the warp direction, including tension, compression, and flexural strength. Interestingly their mechanical properties in the weft direction are about the same. In the through-thickness direction, however, the tensile and flexural strength of 3DOWC is about the same as 3DSBW, both higher than that of 3DSSWC. The compressive strength, on the other hand, is mainly dependent on the number of weft yarns in the through-thickness direction.
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Zhu, Liming, Lihua Lyu, Xuefei Zhang, Ying Wang, Jing Guo, and Xiaoqing Xiong. "Bending Properties of Zigzag-Shaped 3D Woven Spacer Composites: Experiment and FEM Simulation." Materials 12, no. 7 (April 1, 2019): 1075. http://dx.doi.org/10.3390/ma12071075.

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Conventionally laminated spacer composites are extensively applied in many fields owing to their light weight. However, their impact resistance, interlaminar strength, and integrity are poor. In order to overcome these flaws, the zigzag-shaped 3D woven spacer composites were rationally designed. The zigzag-shaped 3D woven spacer fabrics with the basalt fiber filaments tows 400 tex (metric count of yarn) used as warp and weft yarns were fabricated on a common loom with low-cost processing. The zigzag-shaped 3D woven spacer composites were obtained using the VARTM (vacuum-assisted resin transfer molding) process. The three-point bending deformation and effects of damage in zigzag-shaped 3D woven spacer composites were studied both in experiment and using the finite element method (FEM). The bending properties of zigzag-shaped 3D woven spacer composites with different direction, different numbers of weaving cycle, and different heights were tested in experiments. In FEM simulation, the geometrical model was established to analyze the deformation and damage based on the 3D woven composite structure. Compared with data obtained from the experiments and FEM simulation, the results show good agreement and also prove the validity of the model. Based on the FEM results, the deformation, damage, and propagation of stress obtained from the model are very helpful in analyzing the failure mechanism of zigzag-shaped 3D woven composites. Furthermore, the results can significantly guide the fabrication process of real composite materials.
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Lu, Huaiyu, Licheng Guo, Gang Liu, and Li Zhang. "A progressive damage model for 3D woven composites under compression." International Journal of Damage Mechanics 28, no. 6 (August 22, 2018): 857–76. http://dx.doi.org/10.1177/1056789518793994.

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A progressive damage model is proposed to investigate the damage initiation and evolution of 3D woven composites under uniaxial compression at a micromechanical level. The typical compressive experiments were carried out. Based on the observations, the compression failure modes of 3D woven composites mainly include fiber kinking, transverse failure of fiber tow, matrix fracture, and interfacial debonding. The initial damage criteria are according to the physically based failure criteria for the fiber kinking, the Puck criteria for the transverse failure of fiber tow, and the maximum stress criterion for the matrix. The damage of fiber tow–matrix interfacial is simulated through cohesive contact. Particularly, the fiber’s initial misalignment angle is taken into account in the damage model. The simulated compression results agree well with the experimental ones. The compressive stress–strain response of the 3D woven composite is forecasted. The damage evolution of each constituent of the 3D woven composite is obtained. The results show that the influence of the fiber’s initial misalignment angle on the compression strength of the 3D woven composite needs to be considered.
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Jiang, Jiasong, Chunxiao Liao, and Luoqing Zhou. "Development and anti-bending behavior of a ‘π’ shape 3D woven composite." Journal of Reinforced Plastics and Composites 31, no. 5 (March 2012): 351–61. http://dx.doi.org/10.1177/0731684412437268.

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Hollow woven composites are widely used as matrix in aeronautics and vehicles. This paper develops a new ‘π’ shape of 3D woven hollow composite to optimize its bending property. The new structure composite is woven with overlapping warp integral panel enhancing method. In order to weave it out, a new structure of heald has been innovated. Three specimens with different thickness of panels are manufactured by this method. The anti-bending performances of the composites are carried out by four-point bending tests. The experimental results show that with an increase of the number of the composites layers, the Young's modulus and failure loads of the composites are increased significantly.
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Bilisik, Kadir. "Multiaxis 3D Woven Preform and Properties of Multiaxis 3D Woven and 3D Orthogonal Woven Carbon/Epoxy Composites." Journal of Reinforced Plastics and Composites 29, no. 8 (May 27, 2009): 1173–86. http://dx.doi.org/10.1177/0731684409103153.

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Wu, Xiaochuan, Zhongde Shan, Feng Liu, and Yuan Wang. "Mechanical properties of 3D-woven composites with guide sleeves." Journal of Composite Materials 54, no. 12 (March 23, 2016): 1571–78. http://dx.doi.org/10.1177/0021998316636461.

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In this study, the preforms of 3D woven composite materials were made by a flexible oriented 3D composite woven process. The vacuum-assisted resin infusion (VARI) process was used to impregnate the preforms. The short-beam shear test, the compression test, and SEM were used to investigate the interlaminar shear performance and the compression behavior of the 3D woven composite with guide sleeves, and the effect of the guide sleeves on the above properties. It is indicated that the interlaminar shear behavior of 3D woven composites with guide sleeves showed the typical fracture characteristics of a pseudoplastic material. And the fracture modes of interlaminar shear mainly include interlaminar shear fracture and tensile fracture of fibers at the bottom. The interlaminar shear strength of materials increased with the diameter and interval of guide sleeves decreasing. Furthermore, the loss of in-plane compression properties of the materials brought by guide sleeves could be effectively avoided by reasonable control of the diameter and the volume fracture of guide sleeves.
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Dissertations / Theses on the topic "3D WOVEN COMPOSITES"

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Stig, Fredrik. "3D-woven Reinforcement in Composites." Doctoral thesis, KTH, Lättkonstruktioner, 2012. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-70438.

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Composites made from three-dimensional (3D) textile preforms can reduce  both the weight and manufacturing cost of advanced composite structures  within e.g. aircraft, naval vessels and blades of wind turbines. In this thesis composite beams reinforced with 3D weave are studied, which are intended for use as joining elements in a boltless modular design.  In practice, there are a few obstacles on the way to realise the modular boltless design. There is lack of experimental data and more importantly, lack of experience and tools to predict the properties of composites reinforced with 3D-weaves. The novel material will not be accepted and used in engineering applications unless proper design methods are available.  The overall aim of this thesis is to remedy these deficiencies by generating data, experience and a foundation for the development of adequate design methods.  In Paper A, an initial experimental study is presented where the mechanical properties of 3D-weave reinforced composites are compared with corresponding properties of 2D-laminates. The conclusion from Paper A is that the out- of-plane properties are enhanced, while the in-plane stiffness and strength is reduced.  In Paper B the influential crimp parameter is investigated and three analytical models are proposed. The warp yarns exhibit 3D crimp which had a large effect the predicted Young’s modulus as expected. The three models have different levels of detail, and the more sophisticated models generate more reliable predictions. However, the overall trends are consistent for all models.  A novel framework for constitutive modelling of composites reinforced with 3D-woven preforms is presented in Papers C and D. The framework enables predictive modelling of both internal architecture and mechanical properties of composites containing 3D textiles using a minimum of input parameters. The result is geometry models which are near authentic with a high level of detail in features compared with real composite specimens. The proposed methodology is therefore the main contribution of this thesis to the field of composite material simulation.  Paper E addresses the effect of crimp and different textile architectures on the mechanical properties of the final composite material. Both stiffness and strength decreases non-linearly with increasing crimp. Furthermore specimens containing 3D-woven reinforcement exhibit non-linear stress-strain behaviour in tension, believed to be associated with relatively early onset of matrix shear cracks.

QC 20120131

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El, Said Bassam Sabry Fawzy. "Integrated multi-scale modelling of 3D woven composites." Thesis, University of Bristol, 2016. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.720811.

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King, Robert Scott. "Damage tolerant 3D woven technical textiles in reinforced composites." Thesis, University of Ulster, 2010. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.516537.

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Arshad, Mubeen. "Damage tolerance of 3D woven composites with weft binders." Thesis, University of Manchester, 2014. https://www.research.manchester.ac.uk/portal/en/theses/damage-tolerance-of-3d-woven-composites-with-weft-binders(2b1435bc-fdb7-47c3-b555-ca5ea2883b4b).html.

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3D woven composites, due to the presence of through-thickness fibre bridging, have the potential to improve damage tolerance and at the same time to reduce the manufacturing costs. However, the ability to withstand damage depends on weave architecture as well as the geometry of individual tows. A substantial amount of research has been performed to understand in-plane properties as well as the performance of 3D woven composites exposed to impact loads, but there is limited research on the damage tolerance and notch sensitivity of 3D weaves and no work is reported on the damage tolerance of 3D weaves with a weft binding pattern. In view of the recent interest in 3D woven composites, the influence of weft binder on the tensile, open hole tensile, impact resistance and subsequent residual compressive strength properties and failure mechanisms of 3D woven composites was investigated against equivalent UD cross-ply laminate. Four different 3D woven architectures; layer-to-layer, angle interlocked, twill angle interlock and modified angle interlock structures were produced under identical weaving conditions. All the above mentioned tests were performed in both the warp and weft directions on 3D woven and UD cross-ply laminates. Stress concentration and yarn waviness due to through-thickness reinforcement led to lower mechanical properties compared with the UD cross-ply laminate. However, improved in-plane and damage tolerance properties of 3D woven composites under tensile loads were achieved by modifying the weave architecture. The influence of the weave architecture and binder yarn orientation on the notch insensitivity and damage tolerance of 3D woven composites was less significant for compressive loads. Despite the lower undamaged compression strength of 3D woven structures, their residual compressive strength was found to be superior to their equivalent UD cross-ply laminates. The lower rate of strength reduction in the 3D woven fabrics laminates was attributed to a crack bridging mechanism, effectively inhibiting delamination propagation.
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Dai, Shuo. "Mechanical characterisation and numerical modelling of 3D woven composites." Thesis, Loughborough University, 2014. https://dspace.lboro.ac.uk/2134/16221.

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Three-dimensional woven composites were developed to improve the through-thickness properties which conventional two-dimensional laminate composites currently lack. However, these textile composites generally show lower in-plane mechanical properties due to fibre crimping, and also encounter modelling difficulties due to the complex geometries. In this thesis, the static and fatigue mechanical behaviour of several types of 3D woven composites were experimentally characterised, the influence of the weave architecture on the mechanical performance was revealed, and meso/macro scale numerical models with improved failure criteria were developed to simulate the tensile behaviour of the 3D woven composites. The mechanical characterisation was conducted on six woven structures under tension, compression, and flexural loading, and were also carried out on two weaves under open-hole quasi-static tensile and fatigue loading. Digital image correlation and thermoelastic stress analysis were used to characterise the strain and damage development during static and fatigue loading. The testing results showed that the angle-interlock weave W-3 had higher in-plane quasi-static properties, lower notch sensitivity, higher fatigue damage resistance, but lower delamination resistance. The meso-scale model was developed on the unit cell of the woven structure and the macro-scale model (mosaic model) was created on the testing samples. Both un-notched and notched tensile behaviour were modelled for the angle-interlock weave W-3 and a one-by-one orthogonal weave W-1, and the difference between the predicted and experimental results was within 16% for the unit cell models and within 21% for the mosaic models. A modified failure criterion was developed to better simulate the damage behaviour of the notched macro-scale model and improved the predicted notched strength by 10-20%. Whilst further experimental investigation and improvement in the modelling techniques are still required, the data presented in this thesis provided an essential update for the current 3D woven composites research, and the presented models offered the potential to predict the damage behaviour of large 3D woven structures.
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Stig, Fredrik. "An Introduction to the Mechanics of 3D-Woven Fibre Reinforced Composites." Licentiate thesis, Stockholm : Skolan för teknikvetenskap, Kungliga Tekniska högskolan, 2009. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-10235.

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Green, Steven Daniel. "Modelling preform consolidation and its effects in 3D woven composites." Thesis, University of Bristol, 2016. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.705451.

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Broderick, John. "Advancement of 3D woven composites through embedded in situ strain measurement." Thesis, University of Ulster, 2011. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.546738.

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Poole, Matthew C. "Fatigue damage development in 3D woven glass and glass/carbon composites." Thesis, University of Surrey, 2018. http://epubs.surrey.ac.uk/845964/.

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A number of studies have been conducted on 3D non-crimp orthogonal woven composites, but their industrial application is still in its infancy. 3D woven composites show increased through-thickness strength, reducing delamination damage, which is often a key failure mechanism for composites under various loading conditions, especially fatigue. This work investigates the fatigue performance and damage development in a 3D non-crimp orthogonal woven composite consisting of three weft tow layers, two warp tow layers, and a through-thickness z-binder that interlaces along the warp-direction. While the properties of carbon fibres are generally superior to glass fibres, they are more expensive. Therefore, it is of interest to see if the fatigue performance of a glass fibre 3D orthogonal weave can be improved via selective hybridisation using a small amount of carbon fibres. Initial work began on a commercial all-glass 3D orthogonal weave called 3D-78, which was produced by 3TEX. It was found that quasi-static tensile mechanical properties were the same for both warp and weft loading directions, but when loaded in tension-tension fatigue, the warp direction had longer fatigue lifetimes than the weft-direction. The crack density was lower in warp-direction specimens as a result of greater micro-delamination growth blunting stress concentrations around the tips of matrix cracks. The micro-delamination damage in warp-direction fatigue specimens showed a shield-like shape (not previously observed), i.e. wider along one side and narrowing to a point on the other side; where delamination was restricted (at the pointed end), fibre fractures occurred in the adjacent warp tow. The pointed portion of the micro-delamination corresponded to proximity to a z-binder crown. Other damage that was common to both loading directions (warp and weft) included: transverse cracks in transverse tow and resin-rich regions, z-binder debonding, and longitudinal tow splitting cracks. No obvious failure sites were noted for weft-direction fatigue loading. The second material used, 3DMG, was manufactured by the University of Manchester. This material was produced with two different z-binder tensions. The initial z-binder tension (3DMG-T1) resulted in a higher tensile modulus and strength-to-failure, and lower strain-to-failure, for the warp-direction, while the tensile fatigue properties of both directions were similar. Increasing the z-binder tension (3DMG-T2) reduced the tensile modulus and increased the strain-to-failure of the warp-direction, with these properties now similar in both loading directions; the tensile strength for both loading directions remained similar. However, the fatigue performance of the warp-direction was observed to increase with increased z-binder tension, while the weft-direction remained the same. The damage that developed in both materials was similar to the damage in 3D-78, and remained practically the same regardless of z-binder tension, though the energy dissipated per cycle for warp-direction specimens was higher in 3DMG-T1, which corresponds well with the lower number of cycles to failure. The final material tested was a University of Manchester hybrid 3D non-crimp orthogonal woven composite, termed 3DMHyb; here the glass fibre z-binder was replaced with carbon fibre; the z-binder tension used here was the same as 3DMG-T2. Generally, the quasi-static properties of this hybrid material were similar in both loading directions, with the exception of the tensile modulus which was approximately 10% higher, indicating that the carbon fibre z-binder may influence low strain properties. Additionally, the properties of 3DMHyb remained similar to 3DMG-T2. For fatigue performance, However, the fatigue lifetime to failure appeared to increase by a factor of just over 2 at lower peak stress/initial peak strains for the hybrid warp-direction specimens. Again, the energy dissipation per cycle was lower for specimens that had larger number of cycles to failure, in this case the hybrid specimens. Damage development also remained similar between the 3DMG-T2 and 3DMhyb specimens, indicating that the extension of fatigue life noted in 3DMHyb may be the result of the carbon fibre z-binder supressing the development of damage mechanisms leading to ultimate failure of the specimens.
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Waterton, Taylor Lindsey. "Design and manufacture of 3D nodal structures for advanced textile composites." Thesis, University of Manchester, 2007. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:151244.

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Traditional weaving technologies have been utilised over the past twenty-to-thirty years in producing woven textile components that meet engineering requirements through the interlacement of high performance yarns such as carbon, glass and Kevlar. The end performance properties and lightweight characteristics of these fabrics have been adapted within the development of both flat multilevel and shaped configurations for the composites industry. The purpose of the present research required the employment of conventional weaving technologies with limited modifications for the production of 3D woven textile preforms in a variety of truss like configurations; therefore, generating a generic procedure for all yarn combinations and strut and node dimensions for production on dissimilar jacquard looms. The ultimate driving force behind the research was to produce a truss like configuration for the aerospace industry incorporating the design criterion of solid and hollow woven counterparts. This would enable the end truss configuration to have two functions; the first being a lightweight structure by the elimination of bonding applications, through the utilisation of a fully integrated fabrication process; secondly to incorporate hollow struts for a novel storage solution.
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Book chapters on the topic "3D WOVEN COMPOSITES"

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Couégnat, G., E. Martin, and J. Lamon. "3D Multiscale Modeling of the Mechanical Behavior of Woven Composite Materials." In Mechanical Properties and Performance of Engineering Ceramics and Composites V, 185–94. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2010. http://dx.doi.org/10.1002/9780470944127.ch19.

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Judawisastra, H., J. Ivens, and I. Verpoest. "Bending Fatigue Behaviour of PUR-Epoxy and Phenolic 3D Woven Sandwich Composites." In Mechanics of Sandwich Structures, 287–94. Dordrecht: Springer Netherlands, 1998. http://dx.doi.org/10.1007/978-94-015-9091-4_34.

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Koutsonas, Spiridon, and Hasan Haroglu. "Computational Optimization of Voids on 3D Woven Composites Truss Structures During Infusion." In Lecture Notes in Networks and Systems, 326–36. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-80119-9_18.

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Ahmed, Sohail, Xitao Zheng, Tianchi Wu, and Nadeem Ali Bhatti. "Meso-Scale Damage Modeling of Hybrid 3D Woven Orthogonal Composites Under Uni-Axial Compression." In Lecture Notes in Mechanical Engineering, 816–26. Singapore: Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-8331-1_64.

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Eberling-Fux, N., R. Pailler, A. Guette, Sebastien Bertrand, and Eric Philippe. "Impregnation of 3D Woven Carbon Fibre Preforms by Electrophoretic Deposition of Single and Mix of Non Oxide Ceramic Nanoscale Powders, and Densification of the Composite Material." In Advanced Inorganic Fibrous Composites V, 91–96. Stafa: Trans Tech Publications Ltd., 2006. http://dx.doi.org/10.4028/3-908158-06-0.91.

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Legin, B., Z. Aboura, F. Bouillon, and S. Denneulin. "Damage Analysis in 3D Woven SiC/SiC Ceramic Matrix Composite." In Ceramic Transactions Series, 261–71. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2017. http://dx.doi.org/10.1002/9781119407270.ch26.

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Tong, Liyong, Adrian P. Mouritz, and Michael K. Bannister. "3D Woven Composites." In 3D Fibre Reinforced Polymer Composites, 107–36. Elsevier, 2002. http://dx.doi.org/10.1016/b978-008043938-9/50017-x.

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Hallett, Stephen R., Steve D. Green, and Bassam S. F. El Said. "MODELLING 3D WOVEN COMPOSITE PREFORM DEFORMATIONS." In Woven Composites, 141–58. IMPERIAL COLLEGE PRESS, 2015. http://dx.doi.org/10.1142/9781783266180_0004.

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Islam, M. Amirul (Amir). "3D woven preforms for E-textiles and composites reinforcements." In Advances in 3D Textiles, 207–63. Elsevier, 2015. http://dx.doi.org/10.1016/b978-1-78242-214-3.00009-7.

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Ivanov, Dmitry S., and Stepan V. Lomov. "Modeling of 2D and 3D woven composites." In Polymer Composites in the Aerospace Industry, 23–57. Elsevier, 2020. http://dx.doi.org/10.1016/b978-0-08-102679-3.00002-2.

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Conference papers on the topic "3D WOVEN COMPOSITES"

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CHERUET, ANTHONY, and BOBBY COOK. "Material Simulation’s Advantage: An illustration with 3D Woven." In American Society for Composites 2018. Lancaster, PA: DEStech Publications, Inc., 2018. http://dx.doi.org/10.12783/asc33/25934.

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Tayong, Rostand B., Martin J. Mienczakowski, and Robert A. Smith. "3D ultrasound characterization of woven composites." In 44TH ANNUAL REVIEW OF PROGRESS IN QUANTITATIVE NONDESTRUCTIVE EVALUATION, VOLUME 37. Author(s), 2018. http://dx.doi.org/10.1063/1.5031603.

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Oddy, C., M. Ekh, and M. Fagerstrom. "Phase-field Based Damage Modelling of 3D-Woven Composites." In VIII Conference on Mechanical Response of Composites. CIMNE, 2021. http://dx.doi.org/10.23967/composites.2021.084.

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WANG, YOUQI, BINGHUI LIU, LUN LI, AARON TOMICH, and CHIAN FONG YEN. "CAD/CAM Tool for 3D Woven Textile Fabric Design." In American Society for Composites 2017. Lancaster, PA: DEStech Publications, Inc., 2017. http://dx.doi.org/10.12783/asc2017/15209.

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Goering, Jon, and Harun Bayraktar. "3D Woven Composites for Energy Absorption Applications." In SAE 2016 World Congress and Exhibition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2016. http://dx.doi.org/10.4271/2016-01-0530.

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PINEDA, EVAN J., BRETT A. BEDNARCYK, TRENT M. RICKS, BABAK FARROKH, and WADE JACKSON. "Multiscale Failure Analysis of a 3D Woven Unit Cell Containing Defects." In American Society for Composites 2020. Lancaster, PA: DEStech Publications, Inc., 2020. http://dx.doi.org/10.12783/asc35/34928.

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Siddgonde, Nagappa, and Anup Ghosh. "Thermo-Mechanical Modeling of 3D Woven Fabric Composites Using Two-Step Homogenization Approach." In ASME 2019 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2019. http://dx.doi.org/10.1115/imece2019-10913.

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Abstract:
Abstract A 3D finite element based Representative Volume Element (RVE) model has been developed to predict the thermo-mechanical properties of 3D orthogonal interlock woven fabric composites (OIWFC) and angle interlock woven fabric composite (AIWFC) using a two-step homogenization approach. The first step homogenization, micro-homogenization, deals with resin infiltration effect of yarn as a unidirectional continuous fiber with an assumption of 80 percent of fiber volume fraction based on initial fiber and matrix properties. The second step, meso-homogenization, predicts effective thermo-mechanical properties of 3D woven fabric composites based on effective yarn and matrix properties. The RVE analysis has been performed using 3D FEA method with periodic boundary conditions (PBCs). Further, a void study has been performed considering the influences of void on thermo-mechanical properties of the 3D woven fabric composite. It is noted that the influence of void contents plays a significant role in predicting the thermo-mechanical properties of the 3D WFC. The thermo-mechanical properties gradually decrease with an increase of void contents. Studies have been carried out considering the same fiber volume fractions in both 3D WFC models. An AIWFC model predicts higher values of thermo-mechanical constants than OIWFC model.
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El Said, B., and S. Hallett. "Non-Periodicity Challenges in Modelling and Experimental Testing of 3D Woven Composites." In VIII Conference on Mechanical Response of Composites. CIMNE, 2021. http://dx.doi.org/10.23967/composites.2021.071.

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Thuruthimattam, B., and N. Naik. "Mechanical characterization of hybridized 3D orthogonally woven composites." In 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1998. http://dx.doi.org/10.2514/6.1998-1809.

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Yen, Chian-Fong, and Benjamin Boesl. "Progressive Failure Micromechanical Modeling of 3D Woven Composites." In 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2011. http://dx.doi.org/10.2514/6.2011-1796.

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Reports on the topic "3D WOVEN COMPOSITES"

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Yen, Chian-Fong, and Anthony A. Caiazzo. 3D Woven Composites for New and Innovative Impact and Penetration Resistant Systems. Fort Belvoir, VA: Defense Technical Information Center, July 2001. http://dx.doi.org/10.21236/ada393077.

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