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Dissertations / Theses on the topic 'Woven composite'

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Published: 4 June 2021

Last updated: 26 July 2025

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1

Mahadik, Yusuf. "Investigating 3D woven composite architecture." Thesis, University of Bristol, 2011. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.557959.

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Composite parts reinforced with unidirectional or 2D woven reinforcements have been widely used for many years in numerous industries from aerospace to automotive parts. Although their use is widespread, laminated reinforcements have some significant weaknesses that limit their usefulness, including poor interlaminar strength and high cost driven by the need for lengthy hand lay-up to create complex parts. Considerable effort has been put into developing three-dimensional composite reinforcement in order to alleviate these problems. This thesis focuses on materials produced via the weaving met

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2

Marsden, William M. "Damage accumulation in a woven fabric composite." Thesis, University of Surrey, 1996. http://epubs.surrey.ac.uk/844139/.

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Damage development in transparent woven glass fibre reinforced epoxy laminates manufactured from two different commercial cloths has been investigated under quasi-static and cyclic loading. Of the two different cloths, one was woven using untwisted fibre bundles, the second cloth was woven using a fibre bundle which was formed by twisting three smaller bundles together. All laminates were fabricated using a wet lay-up process to impregnate two layers of cloth prior to curing. Uniaxial quasi-static tension and tension-tension fatigue tests were carried out on coupons from both sets of laminates

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3

Foroutan, Rana. "High strain rate behaviour of woven composite materials." Thesis, McGill University, 2010. http://digitool.Library.McGill.CA:8881/R/?func=dbin-jump-full&object_id=92165.

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4

Karaveli, Keriman. "Tribological Properties Of Atightly Woven Carbon-carbon Composite." Master's thesis, METU, 2005. http://etd.lib.metu.edu.tr/upload/12606132/index.pdf.

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ABSTRACT TRIBOLOGICAL PROPERTIES OF A TIGHTLY WOVEN CARBON/CARBON COMPOSITE Karaveli, Keriman M.Sc., Department of Metallurgical and Materials Engineering Supervisor: Prof. Dr. Abdullah &Ouml<br>zt&uuml<br>rk June 2005, 77 pages Tribological properties of a tightly woven Carbon/Carbon (C/C) composite were assessed experimentally in accord with the ASTM pin on disk technique. The C/C composite used in this study was a commercial material (K-Karb) obtained in a panel form. The composite consists of graphite fiber reinforced graphite matrix developed for aerospace applications. The fiber

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5

Davis, Jill Benea. "Three-dimensional multilayer woven fabrics as composite preforms." Thesis, Georgia Institute of Technology, 1993. http://hdl.handle.net/1853/12437.

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6

Quinn, Justin Patrick. "The characteristics of 3D woven textiles for composite materials." Thesis, University of Ulster, 2004. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.414073.

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7

Saleh, Mohamed. "Electromechanical behaviour of three-dimensional (3D) woven composite plates." Thesis, University of Manchester, 2016. https://www.research.manchester.ac.uk/portal/en/theses/electromechanical-behaviour-of-threedimensional-3d-woven-composite-plates(cd06f8ef-88e0-45dd-be65-3911345212ba).html.

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Three dimensional (3D) woven composites have attracted the interest of academia and industry thanks to their damage tolerance characteristics and automated fabric manufacturing. Although much research has been conducted to investigate their out-of-plane "through thickness" properties, still their in-plane properties are not fully understood and rely on extensive experimentation. The aim of this work is to study the electromechanical behaviour of three different fibre architectures of 3D woven composites "orthogonal (ORT), layer-to-layer (LTL) and angle interlock (AI)" loaded, in three differen

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8

Yang, Bing. "Bending, compression, and shear behavior of woven glass fiber/epoxy composites." Thesis, Georgia Institute of Technology, 1995. http://hdl.handle.net/1853/8710.

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9

Matemilola, Saka Adelola. "Impact damage to composite materials." Thesis, University of Cambridge, 1993. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.319939.

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10

Zhu, Bo. "Sheet forming of woven textile composite preforms : formability and wrinkling /." View abstract or full-text, 2007. http://library.ust.hk/cgi/db/thesis.pl?MECH%202007%20ZHU.

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11

Kulkarni, Shridhar S. "Strain rate response of nano enhanced woven fabric composite beams." Connect to online resource - WSU on-site and authorized users, 2005.

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12

Prigent, Yoann. "A Finite Model of Bi-Stable Woven Composite Tape-Springs." Thesis, KTH, Mekanik, 2011. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-104676.

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The recent development of CubeSat nano-satellites shows that it is an effective way to send a payload onto orbit, as it is a relatively inexpensive and quick access to space. If the small size of these satellites is their main advantage, it is also the principal source of problems when it comes to designing it. The control electronics, electric power system and the payload are limited in mass and have to t in a tiny ten-centimeter cube. The necessity of a compact deployable structure to hold the payload once the satellite reached its orbit is one of the principal subject of study for the desig

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13

Yamanaka, Tadayoshi. "Delamination modelling and toughening mechanism of a woven fabric composite." Thesis, McGill University, 2011. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=104701.

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Efficient and accurate numerical simulation methods for the damage tolerance analysis and fatigue life prediction of fibre reinforced polymers are in high demand in industry. Problems arise in the development of such a simulation method due to the limitations from numerical methods, i.e., delamination modelling, and understanding of damage mechanism of woven fabric composites. In order to provide effective and accurate delamination modelling, a new crack modelling method by using the finite element method is proposed in this study. The proposed method does not require additional degrees-of-fre

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14

Morgan, Margaret. "Geometric modelling of 3-D woven reinforcements in composite materials." Thesis, University of Ulster, 2005. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.423442.

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15

Thibodeau, Elisabeth Gabrielle. "Static and Fatigue Fracture Characterization of Primary and Secondary Bonded Woven E-Glass Composites." Fogler Library, University of Maine, 2007. http://www.library.umaine.edu/theses/pdf/ThibodeauEG2007.pdf.

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16

Chretien, Nicolas. "Numerical Constitutive Models of Woven and Braided Textile Structural Composites." Thesis, Virginia Tech, 2002. http://hdl.handle.net/10919/31902.

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Equivalent, three-dimensional elastic moduli are determined from unit cell models of balanced plain weave, 2D braid, 2D triaxial braid and 4x4 twill textile composite materials consisting of interlaced or intertwined yarns. The yarn paths are modeled with undulation portions, in which one yarn passes over and under one or more yarns, and with straight portions. It is assumed that the centerline of a yarn in the undulation portions is described by the sine function, and that the cross-sectional area of a yarn and the thickness of a yarn, normal to the centerline, are uniform along the centerlin

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17

Roach, Kevin K. "Multi-scale analysis of a 2/2-twill woven fabric composite." Thesis, Monterey, California. Naval Postgraduate School, 2002. http://hdl.handle.net/10945/6030.

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Approved for public release; distribution is unlimited<br>A micro-mechanical unit-cell model was developed for 2/2-twill woven fabric composites. A multi-scale bi-directional micro/macro-mechanical analysis technique was applied to the model in an effort to estimate effective material properties of 2/2-twill composites and decompose the effective stresses (strains) of the woven fabric composite into the stresses (strains) of the tows. When this unit-cell model is incorporated into the multiscale analysis by combining with previously developed modules, the residual strength and stiffness of a l

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18

Mendes, Pedro Augusto Aparecido Eggert. "Numerical prediction of compression after impact behavior of woven composite laminates." Instituto Tecnológico de Aeronáutica, 2013. http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2886.

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This work investigates the numerical prediction of the compression after impact behavior of woven composite laminates. Intralaminar and interlaminar damage prediction of the composites lay-ups are evaluated using a proposed damage model implemented as user defined material on ABAQUS Explicit multipurpose FEM code. The numerical models are developed using finite elements method with two different modeling approaches. The Single Shell Model (SSM) used only shell elements to model the laminates and the delamination effects are neglected. To add the delamination effects on the numerical model the

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19

Wagnecz, Linda. "Mechanical behavior and damage mechanisms of woven graphite- polyimide composite materials." Thesis, Virginia Tech, 1987. http://hdl.handle.net/10919/43831.

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The behavior of 8-harness satin woven Celion 3000/PMR-15 graphite-polyimide was experimentally investigated. Unnotched and center-notched specimens from (0)₁₅, (0)₂₂, and (0,45,0, - 45,0,0, - 45,0,45,0)₂ laminates were tested. Material properties were measured and damage development documented under monotonic tension, sustained incremental tension, and tension-tension fatigue loading. Damage evaluation techniques included stiffness monitoring, penetrant-enhanced X-ray radiography, laminate deply, and residual strength measurement. Material properties of the woven graphite-polyimide were compar

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20

Munden, Daniel Christopher. "Development of a Progressive Failure Model for Notched Woven Composite Laminates." Thesis, Virginia Tech, 2018. http://hdl.handle.net/10919/85058.

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As part of the Composite Technology for Exploration (CTE) project at NASA, woven fabric composites are being investigated for their use in Space Launch System (SLS) hardware. Composites are more difficult to analyze than isotropic materials and require more complex methods for predicting failure. NASA is seeking a method for predicting the damage initiation and propagation of woven fabric composites in order to utilize these materials effectively in SLS hardware. This work focuses on notched woven fabric composites under tensile loading. An analytical model consisting of a macro-level failure

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21

Mirzadeh, Farshad. "Compressive strength and behavior of 8H C3000/PMR15 woven composite material." Diss., Virginia Polytechnic Institute and State University, 1988. http://hdl.handle.net/10919/54337.

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Center-notched and unnotched specimens cut from Celion 3000/PMR15 woven composite panels with 60% fiber volume fraction were tested under quasi-static compressive load to failure at room temperature. Micrographic evidence clearly identifies the mode of compressive failure as fiber kinking. Each fiber in the kink fractures because of a combination of compressive and shear stresses. A post failure mechanism follows the local fiber bundle failures, which completely deforms the material by large cracks. ln center notched specimens, fiber kinks start from the notch and propagate to some distance fr

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22

Zhao, Dongming. "Interlaminar fracture behavior of woven fabric composites and mode III delamination analysis." Diss., Georgia Institute of Technology, 1996. http://hdl.handle.net/1853/10075.

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23

Tung, Peter So Wah. "Design and development of three-dimensional multilayer woven preforms for composites." Thesis, Georgia Institute of Technology, 1989. http://hdl.handle.net/1853/8686.

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24

IVANOV, IVELIN VELIKOV. "METHOD DEVELOPMENT FOR FINITE ELEMENT IMPACT SIMULATIONS OF COMPOSITE MATERIALS." University of Cincinnati / OhioLINK, 2002. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1026312498.

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25

Adluru, Hari Kishore. "A Novel Hip Implant Using 3D Woven Composite Material – Design and Analysis." FIU Digital Commons, 2015. http://digitalcommons.fiu.edu/etd/2318.

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The present research focuses on analyzing the possibility of implementing three dimensional woven composite (3DWC) materials in hip implants. The integration of 3DWCs in hip implants has the possibility to both extend the life-time and improve patient outcomes; by spatially varying mechanical properties to meet both biological needs as well as required mechanical loading. In this study, the bulk material properties of 3DWCs were varied based on woven composite architecture and determined using physics based models, which reflect the realistic geometries of fibers in compaction and preform. The

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26

Gabertan, Michael Yandoc. "A comparison of woven fiber composite models to determine coefficients of thermal expansion." Thesis, Georgia Institute of Technology, 1992. http://hdl.handle.net/1853/17309.

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27

Stepto, Simon. "The effect of fibre volume on the mechanical properties of woven composite materials." Thesis, Queen's University Belfast, 1999. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.314218.

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28

Min, Shengnan. "Engineering design of composite military helmet shells reinforced by continuous 3D woven fabrics." Thesis, University of Manchester, 2016. https://www.research.manchester.ac.uk/portal/en/theses/engineering-design-of-composite-military-helmet-shells-reinforced-by-continuous-3d-woven-fabrics(0cd1faec-1e5b-4d1e-9e38-4220fe8dadc8).html.

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The present research aims at engineering design of military helmet shells with continuous 3D woven fabric reinforcements for improved protection at a lighter weight and a reduced cost. The research was carried out using both the experimental and numerical methods. The results proved that the designed 3D woven wadded through-the-thickness angle interlock (TTAI) fabrics can be successfully moulded as continuous reinforcements for the doubly curved military helmet shells; therefore, costs in pattern cutting in the current composite helmet making process are eliminated. An improved ballistic perfo

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29

Westin, Johan. "Ballistic Impact Properties of Fibre-Reinforced Composite Structures." Thesis, KTH, Farkost och flyg, 2011. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-39676.

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30

TANOV, ROMIL R. "A CONTRIBUTION TO THE FINITE ELEMENT FORMULATION FOR THE ANALYSIS OF COMPOSITE SANDWICH SHELLS." University of Cincinnati / OhioLINK, 2000. http://rave.ohiolink.edu/etdc/view?acc_num=ucin962134920.

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31

Fruhmann, Richard Konrad. "Stress and damage assessment in woven composite materials by means of thermoelastic stress analysis." Thesis, University of Southampton, 2009. https://eprints.soton.ac.uk/72146/.

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The work described in this thesis considers the application of thermoelastic stress analysis (TSA) to assess stresses and damage in woven composite materials. Woven composite materials oer high specic strength and stiness, while being well suited to low cost manufacturing techniques. This makes them a cost eective material for weight critical structural applications. The weave, however, introduces stress concentrations at the meso-scale which are critical to damage initiation. Experimental techniques are therefore required to assess the severity of stress concentrations and damage. TSA is an i

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32

Torun, Ahmet Refah. "Advanced manufacturing technology for 3D profiled woven preforms." Doctoral thesis, Saechsische Landesbibliothek- Staats- und Universitaetsbibliothek Dresden, 2011. http://nbn-resolving.de/urn:nbn:de:bsz:14-qucosa-71966.

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3D textile performs offer a high potential to increase mechanical properties of composites and they can reduce the production steps and costs as well. The variety of woven structures is enormous. The algorithms based on the conventional weaving notation can only represent the possible woven structures in a limited way. Within the scope of this dissertation, a new weaving notation was developed in order to analyze the multilayer woven structures analytically. Technological solutions were developed in order to guarantee a reproducible preform production with commingled hybrid yarns. Terry weavin

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33

Hancock, Steven Garth. "Forming woven fabric reinforced composite materials for complex shaped components : informing manufacture with virtual prototyping." Thesis, University of Bristol, 2006. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.430179.

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34

Panchal, Dhaval. "Failure and damage progression of 3D woven composite structures subjected to out-of-plane loading." Thesis, Loughborough University, 2017. https://dspace.lboro.ac.uk/2134/33284.

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Three-dimensionally woven composites are a relatively new class of material that offer improved out-of-plane performance by including through-the-thickness mechanical reinforcement compared to traditional laminated composite structures. The mechanical properties are highly dependent upon the weave architecture as this dictates the nature of the through the thickness reinforcement and its effect in improving out-of-plane shear strength. A comparison of two testing methods, Short Beam Strength, and Five Point Bending was conducted over a range of span to thickness ratios with the latter found to

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35

Hao, Pei. "Mechanical behaviour of woven composite under multiaxial loading conditions by using a modified arcan fixture." Electronic Thesis or Diss., Amiens, 2019. http://www.theses.fr/2019AMIE0014.

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La connaissance du comportement mécanique des matériaux composites est un challenge scientifique mais également un défi industriel. En effet, il est crucial d'anticiper la réponse du matériau en service et en particulier l'apparition de l'endommagement. Dans ce travail de thèse, un matériau composite tissé en fibres de carbone et matrice époxy est considéré. En particulier, son comportement est étudié sous sollicitations multiaxiales. Un modèle élastoplastique couplé avec l'endommagement a été développé pour caractériser le comportement non linéaire du composite. Un procédé d'infusion sous vid

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36

Soysal, Sercan. "Structural Design, Analysis And Composite Manufacturing Applications For A Tactical Unmanned Air Vehicle." Master's thesis, METU, 2008. http://etd.lib.metu.edu.tr/upload/12609506/index.pdf.

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In this study structural design, analysis and composite manufacturing applications for a tactical UAV, which was designed and manufactured in Aerospace Engineering Department of Middle East Technical University (METU), is introduced. In order to make an accurate structural analysis, the material and loading is modeled properly. Computational fluid dynamics (CFD) was used to determine the 3D pressure distribution around the wing and then the nodal forces were exported into the finite element program by means of interpolation from CFD mesh to finite element mesh. Composite materials which are ma

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37

Cholewa, Nathan. "Debond Buckling of Woven E-glass/Balsa Sandwich Composites Exposed to One-sided Heating." Thesis, Virginia Tech, 2015. http://hdl.handle.net/10919/51225.

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An experimental investigation was undertaken to analyze the behavior of sandwich composite structures exposed to one-sided heating where a debond exists between the unexposed facesheet and core material. Sandwich composites of plain weave E-glass/epoxy facesheets and an end-grain balsa wood core manufactured using the Vacuum Assisted Resin Transfer Molding (VARTM) technique were the only materials analyzed. These were selected due to their current use in naval vessels and the heightened interest in the fire response properties of balsa wood and its utility as a core material. In order to bette

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38

Persson, M. (Maria). "3D woven scaffolds for bone tissue engineering." Doctoral thesis, Oulun yliopisto, 2014. http://urn.fi/urn:isbn:9789526206967.

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Abstract Bone tissue engineering has become a rapidly expanding research area because it offers a promising new approach for bone repair and regeneration. Compared to traditional autograft and allograft procedures, bone tissue engineering techniques based on the use of scaffolding materials in combination with autogenous stem cells can eliminate problems of donor site morbidity associated with the harvest of bone tissue, and its short supply. Clearly, the choices of material as well as a scaffold design that enhance bone regeneration are major challenges in the tissue engineering approach. Fib

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39

Altekin, Ahmet. "Multi-level technique for stiffness and strength calculations of woven fabric composite plate and shell structures." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2001. http://handle.dtic.mil/100.2/ADA395985.

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40

Muller, Laura. "Estimation accélérée des performances en fatigue de matériaux et structures composites thermoplastiques par le suivi de leur auto-échauffement." Thesis, Ecole centrale de Nantes, 2019. http://www.theses.fr/2019ECDN0035/document.

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Cette thèse s’inscrit dans le domaine de la fatigue des matériaux composites. Elle consiste à estimer les performances en fatigue d’un matériau composite thermoplastique tissé, en fibres de carbone et matrice PA66, par des essais d’auto-échauffement. Suite à une caractérisation de l’endommagement du matériau sous chargement monotone par un suivi acoustique, thermique et optique, une campagne d’essais de fatigue est réalisée sur deux configurations du matériau, à 0° et à 45°. Plusieurs méthodes de modélisation de la courbe S-N sont proposées, afin de déterminer la limite de fatigue du matériau.

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41

Bouscarrat, David. "Time-dependent damage in woven-ply thermoplastic composites above glass transition temperature Influence of time-dependent phenomena on translaminar fracture of woven-ply C/PPS laminates above the glass transition temperature." Thesis, Normandie, 2019. http://www.theses.fr/2019NORMIR29.

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Dans les composites associant matrice organique et renfort fibreux, le couplage entre comportements visqueux (viscoélasticité, viscoplasticité) et mécanismes d’endommagement est très peu étudié à l’échelle mésoscopique et se limite principalement à des analyses post-mortem. Pour des applications aéronautiques à haute température (e.g., nacelle de moteur d’avion), la problématique est encore plus complexe. Notamment au sein de stratifiés à matrice thermoplastique haute performance PPS renforcés par des tissus de fibres de carbone. Ces matériaux sont caractérisés par des zones riches en matrice

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42

Azehaf, Ismael. "Modélisation du comportement mécanique et de la perméabilité des renforts tissés." Thesis, Lyon, 2017. http://www.theses.fr/2017LYSEI079.

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La mise en forme des pièces composites par Resin Transfert Molding (RTM) nécessite de maîtriser, en autre, deux étapes clés : la déformation à sec du renfort et l’injection de la résine. Dans une démarche d’optimisation du procédé, la simulation numérique est un outil incontournable. Ces travaux de thèse s’inscrivent dans cette thématique avec deux contributions essentielles : Mésomécanique : les renforts textiles sont des milieux poreux périodiques. Ces caractéristiques incitent à les modéliser à l’échelle mésoscopique, où le modèle géométrique se réduit à un Volume Elémentaire Représentatif

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Yu, Bo. "Damage characterisation of 3D woven glass-fibre reinforced composites under fatigue loading using X-ray computed tomography." Thesis, University of Manchester, 2015. https://www.research.manchester.ac.uk/portal/en/theses/damage-characterisation-of-3d-woven-glassfibrereinforced-composites-under-fatigue-loading-using-xraycomputed-tomography(e4d6ee91-e3f5-4b33-b9e7-4367cbbfcf0c).html.

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In the advanced polymer composites reinforced by 3D woven fibre architectures, tows areinterlaced into through-thickness direction to overcome the problems encountered in theapplications of traditional 2D laminates, such as poor interlaminar toughness anddelamination resistance. The understanding of the influence of fibre architectures on thefatigue performance of 3D woven composites is essential in providing guide for the designof fibre architecture. This PhD project is an in-depth study into the fatigue damagemechanisms of 3D woven composites reinforced by two kinds of fibre architectures,na

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Rouault, Thomas. "Propagation de coupure en fatigue sur composites tissés – Etude expérimentale et modélisation." Thesis, Toulouse, ISAE, 2013. http://www.theses.fr/2013ESAE0018/document.

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Les pales d’hélicoptère sont des structures composites soumises à un chargement cyclique multiaxial, et leur criticité impose de porter une attention particulière à la tolérance aux dommages. Leur revêtement peut potentiellement présenter des criques suite à certains évènements (impact, défaut, foudre). Ces travaux se focalisent sur un matériau de revêtement donné (tissu de verre) et concernent l’étude de la propagation de coupure (crique) sous chargement cyclique. Les sollicitations de service ont amené à considérer la traction et le cisaillement plan. Une étude expérimentale a été menée afin

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Mallikarachchi, H. M. Yasitha Chinthaka. "Thin-walled composite deployable booms with tape-spring hinges." Thesis, University of Cambridge, 2011. https://www.repository.cam.ac.uk/handle/1810/239395.

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Deployable structures made from ultra-thin composite materials can be folded elastically and are able to self-deploy by releasing the stored strain energy. Their lightness, low cost due to smaller number of components, and friction insensitive behaviour are key attractions for space applications. This dissertation presents a design methodology for lightweight composite booms with multiple tape-spring hinges. The whole process of folding and deployment of the tape-spring hinges under both quasi-static and dynamic loading has been captured in detail through finite element simulations, starting f

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Komeili, Mojtaba. "Multi-scale characterization and modeling of shear-tension interaction in woven fabrics for composite forming and structural applications." Thesis, University of British Columbia, 2014. http://hdl.handle.net/2429/46507.

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Woven fiber-reinforced polymer composites have become superior materials of choice in advanced industries such as aerospace, energy and automotive. The low in-plane shear stiffness of woven fabrics provides them with high formability, and hence the characterization of this stiffness is of high impotence. Although it was assumed in the past that a fabric’s shear modulus is merely a function of its shear angle, recent evidences show that this material property is also dependent on other factors such as tension along yarns. However, there are currently difficulties to fully characterize the level

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Mathieu, Sylvain. "Modélisation du comportement mécanique lors du procédé de mise en forme et pyrolyse des interlocks CMC." Thesis, Lyon, INSA, 2014. http://www.theses.fr/2014ISAL0115/document.

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La simulation des procédés de production des composites à renforts tissés est un enjeu majeur pour les industries de pointe, où leur utilisation s’intensifie. La maitrise des procédés d’obtention des composites à matrice et fibres en céramique, notamment les étapes de mise en forme et de pyrolyse, s’avère primordiale. La connaissance et la simulation du comportement mécanique aux différentes étapes est nécessaire pour optimiser les performances des pièces finales. Deux approches de modélisation macroscopique des renforts tissés épais de composite sont détaillées : une approche continue classiq

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Wang, Yu. "Multi-scale investigation and analysis of the friction behavior and wear in the manufacturing of the woven composite reinforcements." Electronic Thesis or Diss., Mulhouse, 2024. http://www.theses.fr/2024MULH7126.

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Dans le processus de fabrication des renforts textiles, la friction entre les fils torsadés joue un rôle clé dans les propriétés mécaniques des composites renforcés de fibres, une friction excessive pouvant les détériorer. Cette étude développe un cadre analytique pour comprendre ce comportement frictionnel. Deux modèles analytiques ont été introduits pour décrire la friction des fils, prenant en compte la dynamique de contact à grande échelle. Les validations expérimentales confirment l'efficacité des modèles, offrant une caractérisation détaillée de la friction dans différentes conditions et

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POGGETTI, ILARIA. "Fabrication induced residual strains in thin composite laminates." Doctoral thesis, Università Politecnica delle Marche, 2018. http://hdl.handle.net/11566/253094.

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La presente ricerca è finalizzata a comprendere sperimentalmente e teoricamente i fattori che influenzano la formazione degli strain residui. Tali strain si verificano durante il processo di cura di lastre composite in fibra di carbonio. Il fenomeno degli strain residui che si sviluppano durante la produzione di materiali compositi in fibra di carbonio è uno dei problemi più significativi dell’Industria. La necessità di componenti di alta qualità per applicazioni avanzate richiede che i processi di produzione siano soggetti a gradi di precisione e monitoraggio sempre crescenti nel tentativo di

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Fazeli, Monireh [Verfasser]. "Technology development for woven node structures with complex geometry and in integral design for fiber-reinforced composite applications / Monireh Fazeli." München : Verlag Dr. Hut, 2017. http://d-nb.info/1128466783/34.

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