Relevant bibliographies by topics / Laminated

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Laminated'

Author: Grafiati
Published: 4 June 2021
Last updated: 15 June 2025

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Journal articles on the topic "Laminated"

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bin Yaakob, Mohd Yuhazri, T. T. T. Jennise, H. Sihombing, Qumrul Ahsan, S. T. W. Lau, and Mohd Imran bin Ghazali. "Gravity Effects on the Density of Laminated Composite due to the Differences in Angle Cured." Applied Mechanics and Materials 465-466 (December 2013): 81–85. http://dx.doi.org/10.4028/www.scientific.net/amm.465-466.81.

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This research is carried out to study the feasibility of the gravity effects on curing position of the laminated composite structures to enhance the curing space needed. Vertical cured laminate having almost similar properties with common horizontal cured laminate able to save much space in composite industry especially for developing Small and Medium Industry (SMI). Horizontal cured laminates filled up spaces in which SMI lack of. Polyesters and E-glass fibers were used as the raw material in this research. Vacuum bagging technique was used to suck out the excess resin during lay-up to avoid
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Marzuki, Haslan Fadli Ahmad, Mawarni Mohamad, Engku Ahmadhilmi Engku Ubaidillah, et al. "Effect of Anodizing on Strength of Carbon-Fibre Aluminium-Laminated Composites." Advanced Materials Research 748 (August 2013): 216–21. http://dx.doi.org/10.4028/www.scientific.net/amr.748.216.

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Fibre-metal-laminated composites that consist of aluminium and carbon fibre/epoxy was widely use in engineering fields such as in aerospace and civil application. An issue arise for this laminate systems is that aluminium surfaces must be treated to ensure the effectiveness of load transfer mechanism in the interfacial region. In this research, the effect of anodized layer on the aluminium surface towards strength of the carbon fibre-aluminium-laminated composites was studied. Aluminium 6061-T6 was anodized using phosphoric acid as electrolyte and different anodizing voltage to produce differe
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Mujahid, Yasir, Nabihah Sallih, Mazli Mustapha, Mohamad Zaki Abdullah, and Faizal Mustapha. "Effects of Processing Parameters for Vacuum-Bagging-Only Method on Shape Conformation of Laminated Composites." Processes 8, no. 9 (2020): 1147. http://dx.doi.org/10.3390/pr8091147.

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Complex composite structures manufactured using a low-pressure vacuum bag-only (VBO) method are more susceptible to defects than flat laminates because of the presence of complex compaction conditions at corners. This study investigates the contribution of multivariate processing parameters such as bagging techniques, curing profiles, and laminate structures on laminates’ shape conformation. Nine sets of laminates were produced with a concave corner and another nine sets with a convex corner, both with a 45° inclined structure. Three-way analysis of variance (ANOVA) was performed to quantify t
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Mori, Ryota, Hiroshi Miyamura, Shiomi Kikuchi, et al. "Hydrogenation Characteristics of Mg Based Alloy Prepared by Super Lamination Technique." Materials Science Forum 561-565 (October 2007): 1609–12. http://dx.doi.org/10.4028/www.scientific.net/msf.561-565.1609.

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In order to improve the hydrogenation property of Mg/Ti laminate composite, Ni was added as a third element. Hydrogen storage properties of the laminated Mg/Ti/Ni alloy films were studied. Laminated Mg/Ti/Ni multilayer alloy films were prepared by cold rolling of stacked Mg, Ti and Ni under ambient conditions. The stacked foils were subjected to repetition of rolling and stacking, resulting in super-laminated foils with the thickness less than 0.3mm, containing more than 15000 layers. Microstructures of the super-laminates were studied by scanning electron microscopy and X-ray diffractometry.
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Zhang, Guo Li, Fu You Wang, Jia Lu Li, Guang Wei Chen, and Li Chen. "The Effect of Splicing Shape and Interval Length on the Failure Mode of Laminated Composites under Tensile Condition." Applied Mechanics and Materials 44-47 (December 2010): 2922–25. http://dx.doi.org/10.4028/www.scientific.net/amm.44-47.2922.

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This paper presents an experimental investigation on the failure modes of glass fiber reinforced 2D woven fabric with ladder splicing laminate composites. On the basis of [0/0/+45/90/-45/90]s ply sequence, six kinds of laminated performs with different splicing interval lengths which were 4mm, 8mm, 12mm respectively and two different splicing shape which were ladder splicing and double vertical line splicing, and a kind of laminated perform with continuous laminates of 2D glass fiber woven fabric were made. By means of RTM molding technology, the technological parameters of RTM processing were
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Kormanikova, Eva, Kamila Kotrasova, Jozef Melcer, and Veronika Valaskova. "Numerical Investigation of the Dynamic Responses of Fibre-Reinforced Polymer Composite Bridge Beam Subjected to Moving Vehicle." Polymers 14, no. 4 (2022): 812. http://dx.doi.org/10.3390/polym14040812.

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In modern industry, heavy traditional materials are being substituted with light and strong fibre-reinforced polymer composite materials. Bridges and railroads made of composite laminates are considerably affected by traffic loads. Therefore, it is very important to analyse this effect which would find practical applications in engineering designs. This paper explains the theoretical formulation that governs the dynamic response of a composite beam subjected to a moving load. The governing equations for the dynamic effect on the laminated composite bridge beam are explained here. The main theo
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Joshi, S. P., and N. G. R. Iyengar. "Optimal Design of Laminated Composite Plates Under Axial Compression." Transactions of the Canadian Society for Mechanical Engineering 9, no. 1 (1985): 45–50. http://dx.doi.org/10.1139/tcsme-1985-0007.

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The study is carried out for the optimum design of laminated fiber reinforced composite plates, subjected to multiple in-plane loadings. Angle-ply laminates with orthotropic laminae are considered. Thickness of plies and corresponding fiber orientations are incorporated as design variables. The constrained optimization problem is transformed into a series of unconstrained optimization problems, using an interior penalty function approach. The results have been obtained for different aspect ratios and uniform biaxial in-plane loading ratios. This study shows that the fiber orientations of the p
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Huang, Zheng-Ming, K. Fujihara, and S. Ramakrishna. "Bending Failure Characterisation of Laminated Beams with Braided Fabric Reinforcement." Advanced Composites Letters 12, no. 3 (2003): 096369350301200. http://dx.doi.org/10.1177/096369350301200301.

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An experimental procedure has been performed in this work to characterise failure behaviour of braided fabric reinforced composite laminates subjected to flexural load. The material system used was carbon/epoxy. The laminated beams were made using eight layers of diamond braid reinforcement. Two braiding angles, i.e., 5° and 15°, were applied. Six beams with laminate arrangements of [5/5/5/5/5/5/5/5], [15/15/15/15/15/15/15/15], [5/5/15/15/15/15/5/5], [15/15/5/5/5/5/15/15], [5/5/15/15/5/5/15/15], and [15/15/5/5/15/15/5/5] were loaded under 4-point bending to their ultimate failure, where the br
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bin Yaakob, Mohd Yuhazri, T. T. T. Jennise, H. Sihombing, N. Mohamad, S. H. Yahaya, and M. Y. A. Zalkis. "Water Absorption and Thickness Swelling of Laminated Composite after Cured at Different Angle." Applied Mechanics and Materials 465-466 (December 2013): 86–90. http://dx.doi.org/10.4028/www.scientific.net/amm.465-466.86.

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Moisture absorption is a very important factor in polymers and composite materials used for hull manufacture and stability in marine environment. High water absorption of the material will affects the mechanical properties and stability in composite. This research is carried out to study the feasibility of the gravity effects on curing position of the laminated composite structures to enhance the curing space needed. Vertical cured laminate having almost similar properties with common horizontal cured laminate able to save much space in composite industry. Horizontal cured laminates filled up
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Dibyajyoti, D., and B. Alfia. "Review on laminated composite plates." Proceedings of the 12th Structural Engineering Convention, SEC 2022: Themes 1-2 1, no. 1 (2022): 83–88. http://dx.doi.org/10.38208/acp.v1.477.

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A composite material is a combination of different material which can be assembled to provide required engineering properties like bending, buckling, stiffness etc. It can give better properties than those of individual components. A lamina is the building block of modern composite laminated structures. A lamina is also known as a ply, or a layer. A laminate has several layers of lamina, or laminae. Since the early years of engineering, various types of laminated composite materials have been used in various engineering fields, such as in aerospace, military and automotive industries that are
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Dissertations / Theses on the topic "Laminated"

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Austin, Travis R. "Laminated PAINT." VCU Scholars Compass, 2018. https://scholarscompass.vcu.edu/etd/5462.

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Though we may not perceive it, we are surrounded by material-in-flux. Inert materials degrade and the events that comprise our natural and social environments causally thread into a duration that unifies us in our incomprehension. Sounds reveal ever-present vibrations of the landscape: expressions of the flexuous ground on which we stand.
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Жигилій, Дмитро Олексійович, Дмитрий Алексеевич Жигилий, Dmytro Oleksiiovych Zhyhylii, Володимир Андрійович Хворост, Владимир Андреевич Хворост, and Volodymyr Andriiovych Khvorost. "Laminated composite plates." Thesis, Видавництво СумДУ, 2004. http://essuir.sumdu.edu.ua/handle/123456789/22944.

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Ramakrishnan, Karthik Ram Engineering &amp Information Technology Australian Defence Force Academy UNSW. "Low Velocity Impact Behaviour of Unreinforced Bi-layer Plastic Laminates." Awarded by:University of New South Wales - Australian Defence Force Academy. Engineering & Information Technology, 2009. http://handle.unsw.edu.au/1959.4/43918.

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Low velocity impact behaviour of bi-layered laminates of acrylic and polycarbonate was investigated using a combination of drop tower impact experiments and explicit finite element analysis in LS-DYNA. Material characterisation tests were conducted in tension and in compression to obtain material properties for input to the material model in the numerical analysis. Quasistatic plate bending tests were conducted at different loading rates to compare the quasistatic response of the materials to the impact behaviour. Impact tests on circular plates of monolithic acrylic and polycarbonate were car
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Deka, Lakshya J. "Quasi-static and multi-site high velocity impact response of composite structures." Birmingham, Ala. : University of Alabama at Birmingham, 2008. https://www.mhsl.uab.edu/dt/2008p/deka.pdf.

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Thesis (Ph. D.)--University of Alabama at Birmingham, 2008.<br>Additional advisors: Krishan K. Chawla, Derrick Dean, Jong-Eun Kim, Mark Weaver. Description based on contents viewed Feb. 9, 2009; title from PDF t.p. Includes bibliographical references.
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Zehnder, Nino. "Global optimization of laminated structures /." Zürich : ETH, 2008. http://e-collection.ethbib.ethz.ch/show?type=diss&nr=17573.

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English, Brian Alan. "Laminated Gas Generator Actuator Arrays." Diss., Georgia Institute of Technology, 2006. http://hdl.handle.net/1853/14074.

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Existing microactuator limitations prevent control of small-scale, spin-stabilized vehicles. These applications require actuators insensitive to shock that have forces on the order of Newtons and millisecond control periods. This research presents batch-fabrication lamination approaches for the realization of large arrays of high-impulse, short-duration gas generator actuators (GGAs), and system implementation approaches to integrate these GGAs into a small-scale, spin-stabilized projectile for the purpose of generating steering forces on the projectile. Electronic packaging and MEMS processin
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Patrick, David G. "Laminated structures for sports mouthguards." Thesis, University of Sheffield, 2005. http://etheses.whiterose.ac.uk/6068/.

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The aims and objectives of this study are to examine the role of mouthguards and the materials that are used for their manufacture, the heating process they undergo during manufacture and how the lamination of different materials into a multi-layered system to form a composite structure may affect the impact absorbing capabilities. The effect of heat on pEVA during the manufacturing process was investigated using an instrumented dropweight impact testing rig and a polariscope to observe internal stress as it was felt that the physical properties of the material could be adversely affected by t
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Hassani, Abolfazl. "Bitumin laminated reinforced concrete pavements." Thesis, University of Westminster, 1992. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.305266.

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Jeong, Han Koo. "Reliability of laminated composite plates." Thesis, University of Southampton, 1999. https://eprints.soton.ac.uk/21869/.

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This thesis deals with reliability analysis of laminated composite plates subjected to transverse lateral pressure loads. Input parameters to strengths of the plates such as applied transverse lateral pressure loads, elastic moduli, geometric and ultimate strength values of the plates are treated as basic design variables, and specific probability distributions are applied to them to take into account the variability nature of these basic design variables. Based on the statistical information on the basic design variables, these variables are pseudo-randomly generated in accordance with the co
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Bloomfield, Mark William. "Efficient optimization of laminated composites." Thesis, University of Bristol, 2010. http://hdl.handle.net/1983/716153ce-1826-4c80-b7fa-369a29f45a9e.

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Books on the topic "Laminated"

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InformationCentre, Laminated Glass, ed. Laminated glass. Laminated Glass Informantion Centre, 1992.

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Mikhasev, Gennadi I., and Holm Altenbach. Thin-walled Laminated Structures. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-12761-9.

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BARCHARTS, INC. Reflexology-Laminated. QuickStudy, 2014.

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BARCHARTS, INC. Anatomy-Laminated. QuickStudy, 2013.

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Smith, Evelyn E. Laminated Woman. Start Publishing LLC, 2016.

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Virtanen, Pirjo Kristiina. Laminated Poster. Klett (Ernst) Verlag,Stuttgart, 1999.

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McNally & co. [from old catalog] Rand. Rand McNally Laminated Atlanta Map (Laminated Rolled Map). Rand McNally & Company, 1997.

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Borch. Austria Laminated Map. Borch, 2006.

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Berndtson, Berndtson &. Peru Laminated Map. 6th ed. Berndtson & Berndtson, 2005.

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Berndtson;Borch. Aruba Laminated Map. Berndtson/Borch, 2006.

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Book chapters on the topic "Laminated"

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Huang, Minchao, Jianjun Wu, Jian Li, and Yuqiang Cheng. "Simulation of the Heating of Laminated Heat Exchanger Core Under Variable Operating Conditions." In Solar Thermal Thruster. Springer Nature Singapore, 2024. http://dx.doi.org/10.1007/978-981-97-7490-6_6.

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AbstractThe laminated heat exchange core is the main part that heats the propellant/working fluid in a solar thermal propulsion (STP) system. In this chapter, through a simulation and analysis of the working process of a heat exchanger core with a laminate structure, the laminate heating characteristics of the STP system under variable operating conditions are obtained.
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Kemp, Alan. "Laminated Sediments." In Encyclopedia of Marine Geosciences. Springer Netherlands, 2014. http://dx.doi.org/10.1007/978-94-007-6644-0_185-4.

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Conway, J. H., and N. J. A. Sloane. "Laminated Lattices." In Grundlehren der mathematischen Wissenschaften. Springer New York, 1988. http://dx.doi.org/10.1007/978-1-4757-2016-7_6.

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Conway, J. H., and N. J. A. Sloane. "Laminated Lattices." In Grundlehren der mathematischen Wissenschaften. Springer New York, 1993. http://dx.doi.org/10.1007/978-1-4757-2249-9_6.

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Conway, J. H., and N. J. A. Sloane. "Laminated Lattices." In Grundlehren der mathematischen Wissenschaften. Springer New York, 1999. http://dx.doi.org/10.1007/978-1-4757-6568-7_6.

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Emary, A. B. "Laminated Components." In Site Carpentry and Advanced Joinery. Macmillan Education UK, 1985. http://dx.doi.org/10.1007/978-1-349-06901-9_20.

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Kumar, Rajesh. "Laminated Sediments." In Encyclopedia of Earth Sciences Series. Springer Netherlands, 2011. http://dx.doi.org/10.1007/978-90-481-2642-2_319.

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Gooch, Jan W. "Laminated, Cross." In Encyclopedic Dictionary of Polymers. Springer New York, 2011. http://dx.doi.org/10.1007/978-1-4419-6247-8_6761.

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Gooch, Jan W. "Laminated Fabric." In Encyclopedic Dictionary of Polymers. Springer New York, 2011. http://dx.doi.org/10.1007/978-1-4419-6247-8_6762.

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Gooch, Jan W. "Laminated Glass." In Encyclopedic Dictionary of Polymers. Springer New York, 2011. http://dx.doi.org/10.1007/978-1-4419-6247-8_6763.

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Conference papers on the topic "Laminated"

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Herman, Mélanie, Christian Hochard, Jean-Marc Besson, Jean-Paul Charles, Nassira Boulebbad-Gomez, and Noël Lahellec. "Development of Techniques for Composite Parts Failure Analysis in Static and Fatigue Mode - Application on Thermoset and Thermoplastic Materials for Rotorcraft Main Rotor Hub Analysis." In Vertical Flight Society 74th Annual Forum & Technology Display. The Vertical Flight Society, 2018. http://dx.doi.org/10.4050/f-0074-2018-12887.

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A model defined at the ply scale to predict the failure of laminated composites for static or fatigue loading is proposed. The model describes the loss of strength in the fiber direction for a significant level of transverse damage. This meso-scale model has been characterized on woven ply laminates used for rotorcraft dynamic components, such as glass/epoxy of Starflex®, carbon fiber/epoxy, and carbon fiber/PEEK of H160 main rotor hub. Failure behavior prediction at coupon level has been validated regarding static and fatigue failure mode in tension for epoxy resin woven ply laminates. Charac
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He, Xiaoling. "Nonlinear Thermal Vibration Analysis of a Thin Laminated Microstructure." In ASME 2005 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. ASMEDC, 2005. http://dx.doi.org/10.1115/detc2005-85326.

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Nonlinear deformation can occur in thin laminated structures due to thermal fields present in the laminates. Thermally induced laminate response in buckling and vibration has been previously studied in nonlinear dynamics by approximations that compromise the total energy of the system. In this paper, this problem is studied based on the nonlinear thermal mechanical analysis of a thin laminated structure using a Galerkin type approach, with total energy conservation. Equation of motion for laminates in orthotropic and isotropic structures in thermal buckling response in a simply supported bound
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Nandi, Soumitra, Zahed Siddique, and Cengiz Altan. "A Customization Approach for Design Using Commercially Available Laminated Composite Materials." In ASME 2011 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. ASMEDC, 2011. http://dx.doi.org/10.1115/detc2011-48461.

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Composite materials can offer wide range of thermo-mechanical properties when designing load bearing components using them. The wide range of properties can be obtained by varying fiber-matrix volumetric ratio. Another advantage of using composite materials in design is that the directional properties of laminated composite materials can be easily manipulated by varying the angle of orientation with respect to the direction of the load. Theoretically it is possible to design composite laminates with any fiber-matrix ratio, and in any orientation. But in practice, only a selective number of lam
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Christoph, Jake E., Colin M. Gregg, Jordan R. Raney, and David A. Jack. "Low Velocity Impact Testing of Laminated Carbon Fiber/Carbon Nanotube Composites." In ASME 2015 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2015. http://dx.doi.org/10.1115/imece2015-52984.

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Carbon fiber laminated thermoset composites have become the industry standard for applications dictating a high strength-to-weight ratio. However, the brittle nature of the carbon fiber composite structure limits its energy dissipation characteristics, often leading to catastrophic failure under low energy impact loadings. This research examines the potential effects of including vertically aligned multi-walled carbon nanotube forests within a layered laminate structure with the goal being to increase the energy dissipation of the structure with attention given to the increase in the aerial de
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Ye, R., H. S. Tzou, and J. Tani. "Control of Semicircular Shells With Thermal Shock and Mechanical Excitations." In ASME 1996 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 1996. http://dx.doi.org/10.1115/imece1996-0937.

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Abstract Shell-type components and structures are very common in many mechanical and structural systems, e.g., nozzles, pressure vessels, storage tanks, rockets, antenna dishes, etc. Modeling and analysis of adaptive piezothermoelastic shell laminates represents a high level of sophistication and complexity. Accordingly, a numerical method is developed to investigate the complicated temperature, mechanical, and control interactions of piezothermoelastic shell composites in this study. Constitutive equations, governing equations, and boundary conditions of a generic piezothermoelastic continuum
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Allen, David H., and Chad R. Searcy. "Modeling Damage Accumulation in Laminated Composites Subjected to Impact." In ASME 2000 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2000. http://dx.doi.org/10.1115/imece2000-1962.

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Abstract Because of their high strength-to-weight ratio, laminated composites continue to be an attractive alternative to conventional monolithic media in the design of impact resistant structures. Unfortunately, the high cost of production has been a major limiting factor in the usage of laminated composites in design applications. Contributing to this cost is the complexity of the design process, which calls for an increased number of parameters necessary for the optimal design of impact resistant laminated composite structures. One way to address this complexity is through the use of damage
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Jung, Dongho, Hyeonju Kim, Moonho Tak, Kyungjae Lee, and Taehyo Park. "Dynamic Structural Analysis of a Large-Diameter Riser Consisting of Laminated Composite Material With a Hybrid Numerical Scheme." In ASME 2013 32nd International Conference on Ocean, Offshore and Arctic Engineering. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/omae2013-10868.

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A hybrid numerical scheme is developed to analyze the structural dynamic behavior of a large-diameter riser made of a laminated composite material. The global dynamic behavior of the riser, considered as a beam element subjected to a wave and current, is solved with the finite element analysis method in the time domain. The equivalent elastic modulus of a laminated composite riser for the global dynamic analysis is calculated from the stress-strain relation of a laminate structure with a different elastic modulus. For elements in large displacement and stresses estimated from the dynamic analy
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Vinogradov, Aleksandra M. "Buckling Characteristics of Regular and Irregular Asymmetric Laminated Composites." In ASME 1998 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 1998. http://dx.doi.org/10.1115/imece1998-0883.

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Abstract The paper examines the effects of composite material properties on the nonlinear buckling response of irregular asymmetric composite structures through the analysis of asymmetric laminated beam-columns composed of an arbitrary number of different material layers. The nonlinear buckling behavior of the structures subjected to combined compression and bending is examined as a function of the number, orientation and stacking sequence of the layers that make up the laminate. The analysis demonstrates that, typically, buckling of asymmetric composites is initiated immediately at the load a
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BUENROSTRO, JAVIER, SANDI G. MILLER, TRENTON M. RICKS, and J. MICHAEL PERIERA. "DAMAGE INITIATION OF CONTINUOUS FIBER LAMINATED THERMOPLASTIC COMPOSITES." In Proceedings for the American Society for Composites-Thirty Eighth Technical Conference. Destech Publications, Inc., 2023. http://dx.doi.org/10.12783/asc38/36674.

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The use of advanced thermoplastic composites (TPC) for structural applications in the aerospace and automotive industries has grown increasingly popular due to their high performance, high manufactured part output, and sustainability. Advanced manufacturing processes of thermoplastic composites allow for the building of complex optimized structural geometries with both continuous and discontinuous fibers. With more complex parts and processes comes the need for established qualification methodologies. Characterization of damage evolution from different manufacturing processes needs to be furth
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Viviani, L. "Fractional viscoelastic characterization of laminated glass." In AIMETA 2022. Materials Research Forum LLC, 2023. http://dx.doi.org/10.21741/9781644902431-18.

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Abstract. Glass façades are often required to withstand against explosive events due to premeditated or accidental causes. Laminates made by glass plies bonded by thin polymeric foils (laminated glass) need to be used to avoid catastrophic breakage. The paradigmatic case study considered is that of a rectangular three-layer laminate, made of two glass plies, modelled as Kirchhoff-Love plates, sandwiching a thin viscoelastic polymeric interlayer. Its time-dependent response under the action of a blast wave is described via fractional calculus operators, whose main advantage is that only two mat
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Reports on the topic "Laminated"

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Harris, Chioke, Heather Goetsch, and Swaroop Atnoorkar. Cross-Laminated Timber Workshop: Pathways and Priorities for Cross-Laminated Timber Building Systems. Office of Scientific and Technical Information (OSTI), 2022. http://dx.doi.org/10.2172/1868051.

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Burov, A., and V. Lebedev. Impedances of Laminated Vacuum Chambers. Office of Scientific and Technical Information (OSTI), 2011. http://dx.doi.org/10.2172/1021483.

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Hammerand, Daniel Carl. Laminated composites modeling in ADAGIO/PRESTO. Office of Scientific and Technical Information (OSTI), 2004. http://dx.doi.org/10.2172/919118.

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Thies, Walter G., and Rona N. Sturrock. Laminated root rot in western North America. U.S. Department of Agriculture, Forest Service, Pacific Northwest Research Station, 1995. http://dx.doi.org/10.2737/pnw-gtr-349.

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5

Swab, Jeffrey, and Parimal Patel. Fracture Analysis of a Laminated Window Structure. DEVCOM Army Research Laboratory, 2022. http://dx.doi.org/10.21236/ad1161194.

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Shafer, R. E. Coupling impedance of laminated magnets in the booster. Office of Scientific and Technical Information (OSTI), 1986. http://dx.doi.org/10.2172/5334017.

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Wang, A. S. Fracture Analysis of Matrix Cracking in Laminated Composites. Defense Technical Information Center, 1985. http://dx.doi.org/10.21236/ada170486.

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Hartman, Quinn. MIL-STD-1660 Testing of Laminated Wood Pallets. Defense Technical Information Center, 1989. http://dx.doi.org/10.21236/ada244939.

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Folias, E. S. Failure in Laminated Composite Plates Containing a Hole. Defense Technical Information Center, 1990. http://dx.doi.org/10.21236/ada227307.

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Kotov, Nicholas A. Engineering of High-Toughness Carbon Nanotubes Hierarchically Laminated Composites. Defense Technical Information Center, 2012. http://dx.doi.org/10.21236/ada564047.

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