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Journal articles on the topic 'Multilayred composite plates'

Author: Grafiati

Published: 28 May 2022

Last updated: 31 July 2025

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1

Santo, Loredana, Fabrizio Quadrini, and Denise Bellisario. "Multilayered Composite Plates with Shape Memory Properties." Key Engineering Materials 699 (July 2016): 1–7. http://dx.doi.org/10.4028/www.scientific.net/kem.699.1.

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In this study, multilayered composite plates with shape memory properties were produced: carbon fibers prepreg are alternated with layers of shape memory epoxy powder obtaining composite with different number of layers. The differences in the load exerted during shape recovery, and percentage and time of recovery of the composites as a function of layers number have been evaluated. In particular, the actuation load and the shape recovery percentage were measured after a V-shape memorizing step of the composites. The experimental results are very promising, showing that such multilayers can suc

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2

BRISCHETTO, SALVATORE. "AN EXACT 3D SOLUTION FOR FREE VIBRATIONS OF MULTILAYERED CROSS-PLY COMPOSITE AND SANDWICH PLATES AND SHELLS." International Journal of Applied Mechanics 06, no. 06 (2014): 1450076. http://dx.doi.org/10.1142/s1758825114500768.

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A 3D free vibration analysis of multilayered structures is proposed. An exact solution is developed for the differential equations of equilibrium written in general orthogonal curvilinear coordinates. The equations consider a geometry for shells without simplifications and allow the analysis of spherical shell panels, cylindrical shell panels, cylindrical closed shells and plates. The method is based on a layer-wise approach, the continuity of displacements and transverse shear/normal stresses is imposed at the interfaces between the layers of the structures. Results are given for multilayered

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3

Rao, Ananda M., Ch Ratnam, J. Srinivas, and A. Premkumar. "Optimum design of multilayer composite plates using simulated annealing." Proceedings of the Institution of Mechanical Engineers, Part L: Journal of Materials: Design and Applications 216, no. 3 (2002): 193–97. http://dx.doi.org/10.1177/146442070221600304.

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This paper proposes the use of a simulated annealing (SA) approach to the optimal design of multilayered composite plate structures. The orientation fibres and the number of layers in laminated composites play a major role in determining strength and stiffness. Therefore, the basic design problem is to determine the optimum stacking sequence of the composite laminate. The SA technique is employed to obtain the optimum fibre orientation of multilayered composite plates, so as to maximize fundamental natural frequency. The composite plate is discretized and analysed by a finite element (FE) anal

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Aydaraliev, Zh, M. Abdiev, and Yu Ismanov. "Two-layer Composite Reinforced With Basalt Fibers of Various Lengths." Bulletin of Science and Practice 6, no. 5 (2020): 12–20. http://dx.doi.org/10.33619/2414-2948/54/01.

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The article considers the issues of creating composites using long, continuous structures along the entire length of the structure, and short basalt fibers, and, based on them, multilayer composite materials as reinforcement. A mathematical description of the strength properties of multilayer composite materials based on layers of composites using long, continuous along the entire length of the structure, and short basalt fibers as reinforcement is considered. The results of theoretical studies showed that the multilayer composite material has improved properties. The first layer of material,

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Noor, Ahmed K., and W. Scott Burton. "Computational Models for High-Temperature Multilayered Composite Plates and Shells." Applied Mechanics Reviews 45, no. 10 (1992): 419–46. http://dx.doi.org/10.1115/1.3119742.

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The focus of this review is on the hierarchy of composite models, predictor-corrector procedures, the effect of temperature-dependence of material properties on the response, and the sensitivity of the thermomechanical response to variations in material parameters. The literature reviewed is devoted to the following eight application areas: Heat transfer; thermal stresses; curing, processing and residual stresses; bifurcation buckling; vibrations of heated plates and shells; large deflection and postbuckling problems; and sandwich plates and shells. Extensive numerical results are presented sh

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6

Wei, Z., L. H. Yam, and L. Cheng. "Delamination Assessment of Multilayer Composite Plates Using Model-based Neural Networks." Journal of Vibration and Control 11, no. 5 (2005): 607–25. http://dx.doi.org/10.1177/1077546305052317.

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A procedure for damage detection in multilayer composites is described using model-based neural networks and vibration response measurement. The appropriate finite element model is established to generate the training data of neural networks. Internal delaminations with different sizes and locations are considered as the particular damage scenarios in multilayer composite plates. The damage-induced energy variation of response signal is investigated, and the mechanism of mode-dependent energy dissipation of composite plates due to delamination is revealed. In order to obtain the structural dyn

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7

Noor, Ahmed K., and Jeanne M. Peters. "Thermomechanical Buckling of Multilayered Composite Plates." Journal of Engineering Mechanics 118, no. 2 (1992): 351–66. http://dx.doi.org/10.1061/(asce)0733-9399(1992)118:2(351).

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8

Veerappan, Balasubramani, K. L. Gokulraju, S. Sreenivas, and K. J. Nagarajan. "Failure Analysis in a Multilayerd Glass Fiber Reinforced Polyester Composite Plates under Flexural Loading." Materials Science Forum 1081 (March 24, 2023): 67–81. http://dx.doi.org/10.4028/p-h235pa.

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The usage of laminated glass fiber reinforced polyester composites in aerospace applications helps to reduce overall weight of the aerospace structures. The flexural strength of the laminated glass fiber reinforced composites becomes more important when they are employing for aeroplane wings. In this work, a laminated glass fiber polyester composite with two distinct sets of six different woven lamina stacking sequences is manufactured via hand layup technique. The effect of stacking sequence over the total ply failure load are investigated through universal testing machine. Finally, the progr

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9

Pysarenko, O. "DISPERSION OF LAMB WAVES IN MULTILAYER STRUCTURES." Mechanics And Mathematical Methods 6, no. 2 (2024): 124–35. http://dx.doi.org/10.31650/2618-0650-2024-6-2-124-135.

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Low cost, the possibility of online monitoring and high sensitivity distinguish the method of structural monitoring using Lamb waves from other available methods. Structural analysis based on Lamb waves in heterogeneous materials requires fundamental knowledge of the behavior of Lamb waves in such materials. This basic knowledge is critical for signal processing in determining possible damage that can be detected by the propagating wave. Recently, Lamb wave methods have been used to simultaneously survey large areas of composite structures. However, such methods are more complex than tradition

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10

Dat, Pham Tien, and Nguyen Hoa Thinh. "Some results in studying multilayered composite plates." Vietnam Journal of Mechanics 21, no. 2 (1999): 89–98. http://dx.doi.org/10.15625/0866-7136/9990.

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11

Shih, Cheng-Hung, Jhu-Lin You, Yung-Lung Lee, et al. "Design and Ballistic Performance of Hybrid Plates Manufactured from Aramid Composites for Developing Multilayered Armor Systems." Polymers 14, no. 22 (2022): 5026. http://dx.doi.org/10.3390/polym14225026.

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In this study, the impact resistance of aramid fabric reinforced with shear thickening fluids (STFs), epoxy or polyurea elastomers is examined through ballistic tests. According to the ballistic test results, the aramid composite structure treated with polyurea elastomers absorbs the most impact energy per unit area density and has the best impact resistance. However, the occurrence of stress concentration during ballistic impact reduces the impact resistance of the aramid composite structure treated with epoxy. On the other hand, aramid fabric impregnated with STF improves structural protecti

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12

Ajdour, M., A. Bakkali, L. Azrar, and A. El Omri. "Modeling and analysis of loaded multilayered magnetoelectroelastic structures composite materials: Applications." Advanced Electromagnetics 5, no. 3 (2016): 91. http://dx.doi.org/10.7716/aem.v5i3.426.

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This paper presents the detailed analysis of fiber- reinforced magnetoelectroelastic composite plates. The work is divided into two major sections. The first one deals with the homogenization of the properties of each layer based on the Mori-Tanaka mean field approach where all the needed effective coefficients of each layer are determined. Then, in order to perform analysis of the considered, the Stroh formalism is used to provide solutions for multifunctional multilayered magnetoelectroelastic composites, to predict exactly the mechanical and electrical behaviors near or across the interface

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13

Noor, Ahmed K., and W. Scott Burton. "Assessment of Shear Deformation Theories for Multilayered Composite Plates." Applied Mechanics Reviews 42, no. 1 (1989): 1–13. http://dx.doi.org/10.1115/1.3152418.

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A review is made of the different approaches used for modeling multilayered composite plates. Discussion focuses on different approaches for developing two-dimensional shear deformation theories; classification of two-dimensional theories based on introducing plausible displacement, strain and/or stress assumptions in the thickness direction; and first-order shear deformation theories based on linear displacement assumptions in the thickness coordinate. Extensive numerical results are presented showing the effects of variation in the lamination and geometric parameters of simply supported comp

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Yakubovskiy, Yu E., V. I. Kolosov, A. G. Kuzyaev, and S. O. Kruglov. "Calculation and manufacture of multilayer composite structures." E3S Web of Conferences 474 (2024): 01066. http://dx.doi.org/10.1051/e3sconf/202447401066.

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A brief overview of the work done to solve the problems of bending of composite plates and shells is presented. A mathematical model has been developed that takes into account the physically nonlinear properties of the layer’s material. The seams between the layers have finite longitudinal stiffness. Seams can be continuous or discrete (anchors). The proposed mathematical model makes it possible to take into account the creep properties of the aging material. The reliability of calculations is substantiated by comparison with experimental data and known calculations. Taking into account the te

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15

Kasimov, A. T. "INVESTIGATION OF LAYERED ORTHOTROPIC STRUCTURES BASED ON ONE MODIFIED REFINED BENDING THEORY." Eurasian Physical Technical Journal 18, no. 4 (38) (2021): 37–44. http://dx.doi.org/10.31489/2021no4/37-44.

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In the article, constructions made of orthotropic multilayer composite material, in particular, layered orthotropic plates are considered. Numerical modeling and analysis of the stress-strain state for the plates are carried out on the basis of one version for the refined theory of layered plates. The bending problems for plates of medium thickness and thin multilayer plates of symmetric and asymmetric structures are investigated. All studies are conducted taking into account the properties of orthotropy and multilayering for the composite material from which the plates are made. The general a

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16

Sreekanth, T. G., M. Senthilkumar, and S. Manikanta Reddy. "Artificial neural network based delamination prediction in composite plates using vibration signals." Frattura ed Integrità Strutturale 17, no. 63 (2022): 37–45. http://dx.doi.org/10.3221/igf-esis.63.04.

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Dynamic loading on composite components may induce damages such as cracks, delaminations, etc. and development of an early damage detection technique for delaminations is one of the most important aspects in ensuring the integrity and safety of composite components. The presence of damages such as delaminations on the composites reduces its stiffness and further changes the dynamic behaviour of the structures. As the loss in stiffness leads to changes in the natural frequencies, mode shapes, and other aspects of the structure, vibration analysis may be the ideal technique to employ in this cas

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17

Ben Amor, Morched. "Guided modes modeling in multilayered composites plates." Journal of the Acoustical Society of America 123, no. 5 (2008): 3840. http://dx.doi.org/10.1121/1.2935642.

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18

Zhan, Jian Chao. "Study on the Properties of Polyester Fabric by Ni/Co/Fe Multilayer Electroless Plating Technology." Advanced Materials Research 602-604 (December 2012): 1729–32. http://dx.doi.org/10.4028/www.scientific.net/amr.602-604.1729.

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The Ni/Co/Fe plated fabric was obtained by electroless plating. The surface morphology, crystal structure, composition,surface resistance and microwave absorption performance of Ni/Co/Fe plated PET fabric were investigated. The results show that the composites possess effective microwave absorption. The characteristics of microwave absorption can be controlled by adjusting element ratios in composition. This kind of composite has great potential and investigation value in microwave absorbing fields.

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19

Chan-Colli, Danny G., Eliana M. Agaliotis, David Frias-Bastar, et al. "Ballistic Behavior of Bioinspired Nacre-like Composites." Biomimetics 8, no. 4 (2023): 341. http://dx.doi.org/10.3390/biomimetics8040341.

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In this paper, the ballistic performance of a multilayered composite inspired by the structural characteristics of nacre is numerically investigated using finite element (FE) simulations. Nacre is a natural composite material found in the shells of some marine mollusks, which has remarkable toughness due to its hierarchical layered structure. The bioinspired nacre-like composites investigated here were made of five wavy aluminum alloy 7075-T651 (AA7075) layers composed of ~1.1-mm thick square tablets bonded together with toughened epoxy resin. Two composite configurations with continuous layer

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20

Ousset, Y., and F. Roudolff. "Numerical analysis of delamination in multilayered composite plates." Computational Mechanics 20, no. 1-2 (1997): 122–26. http://dx.doi.org/10.1007/s004660050227.

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21

Dimitrienko, Yu, E. Gubareva, and A. Tumanov. "Modeling of aeroelastic composite plates vibrations based on asymptotic theory." E3S Web of Conferences 376 (2023): 01039. http://dx.doi.org/10.1051/e3sconf/202337601039.

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The paper is devoted to solving the problem of aeroelastic deformation of multilayer thin composite plates. A theory of aeroelastic deformations of composite plates based on the application of the asymptotic averaging method and piston theory for modeling pressure on the body surface is proposed. The averaged equations of aeroelastic vibrations of composite plates are derived. An example of a numerical solution of the problem of one-dimensional bending vibrations of a composite plate based on the developed theory is given.

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22

Geng, Wei, Ye Xiong Qi, and Jia Lu Li. "Bending Properties of Five-Layer Biaxial Weft Knitted Fabric Reinforced Composite Materials." Advanced Materials Research 391-392 (December 2011): 359–63. http://dx.doi.org/10.4028/www.scientific.net/amr.391-392.359.

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Five-layer biaxial weft knitted (FBWK) fabric is one kind of multilayered biaxial weft knitted (MBWK) fabric. FBWK fabric is made of carbon fiber as inserted yarns and stitched with polyester yarns, and it has been impregnated with epoxy via resin transfer molding (RTM) technique to manufacture the composite plates. The bending properties of the FBWK fabric reinforced composite are studied with the three-point bending test method. The bending properties of the FBWK fabric reinforced composite materials with different fiber volume fraction have been investigated. The results show that the relat

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23

Wu, Chih-Ping, and Wei-Chen Li. "Quasi-3D Stability and Vibration Analyses of Sandwich Piezoelectric Plates with an Embedded CNT-Reinforced Composite Core." International Journal of Structural Stability and Dynamics 16, no. 02 (2016): 1450097. http://dx.doi.org/10.1142/s0219455414500977.

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Quasi-three-dimensional (3D) stability and free vibration analyses of bi-axially loaded, simply-supported, sandwich piezoelectric plates with an embedded either a functionally graded (FG) carbon nanotube-reinforced composite (CNTRC) core or a multilayered fiber-reinforced composite (FRC) one are presented. Three different distributions of carbon nanotubes (CNTs) through the thickness of the CNTRC core, i.e. uniformly distributed and FG V-, rhombus- and X-type variations, are considered, and the effective material properties of the CNTRC core are estimated using the rule of mixtures. The Pagano

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24

Kryshchuk, Mykola, Egor Ovcharenko, and Hanna Us. "Determination of elastic characteristics for a package of monolayers thin-walled plates from composite fibrous materials." Mechanics and Advanced Technologies 7, no. 2 (98) (2023): 155–59. http://dx.doi.org/10.20535/2521-1943.2023.7.2.287711.

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An analytical method for calculating the equivalent elastic characteristics of anisotropic multilayer plates made of composite fibrous materials is laid out. The main assumptions taken into consideration when calculating elastic moduli and Pousson's coefficients are that fibers are elastic materials with orthotropic mechanical characteristics that deform together when multilayer plates are loaded. Analytical methods for calculating effective modulus of elasticity most common in practical applications of applied mechanics are laid out in the list of cited publications. These include the rules o

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25

Bezerra, Wendell B. A., Benjamin S. Lazarus, Ulisses O. Costa, et al. "Energy Absorption and Ballistic Performance of Epoxy Composite Reinforced with Arapaima Scales." Polymers 15, no. 7 (2023): 1614. http://dx.doi.org/10.3390/polym15071614.

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Arapaima scales possess a hierarchical structure capable of absorbing a considerable amount of energy before fracture. These natural dermal armors present significant potential in the sustainable development of cost-effective composites. This work aimed, for the first time, to analyze the impact resistance and ballistic performance of arapaima scale-reinforced epoxy composites and their potential application in multilayered armor systems (MAS). Composite plates were prepared with 20%, 30%, and 40 vol% of arapaima scales. Composite specimens were subjected to notched Izod impact and residual ve

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26

Krivenko, Olga P., Petro Lizunov, Yurii Vorona, and Oleksandr Kalashnikov. "Modeling of thermo-elastic properties of composite material in stability problems of multilayered shells." Management of Development of Complex Systems, no. 54 (June 2, 2023): 77–89. http://dx.doi.org/10.32347/2412-9933.2023.54.77-89.

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Thin-walled structures, the elements of which are plates and shells made of composite materials, are increasingly used in various industries. The growing needs of practice and the introduction of new composite materials require further improvement of the calculation methods of shell structures of inhomogeneous structure. Therefore, the problem of developing an adequate method of analyzing the behavior of shells made of composite materials with a multilayer structure is relevant. The work is devoted to the application of the developed method of finite elements for the analysis of geometrically

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Lizunov, Petro, and Valentyn Nedin. "Numerical study of transmission shafts dynamics in motion modes when the rotation speed changes." Management of Development of Complex Systems, no. 55 (September 25, 2023): 117–22. http://dx.doi.org/10.32347/2412-9933.2023.55.117-122.

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Thin-walled structures, the elements of which are plates and shells made of composite materials, are increasingly used in various industries. The growing needs of practice and the introduction of new composite materials require further improvement of the calculation methods of shell structures of inhomogeneous structure. Therefore, the problem of developing an adequate method of analyzing the behavior of shells made of composite materials with a multilayer structure is relevant. The work is devoted to the application of the developed method of finite elements for the analysis of geometrically

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28

Pan, E. "Exact Solution for Simply Supported and Multilayered Magneto-Electro-Elastic Plates." Journal of Applied Mechanics 68, no. 4 (2001): 608–18. http://dx.doi.org/10.1115/1.1380385.

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Exact solutions are derived for three-dimensional, anisotropic, linearly magneto-electro-elastic, simply-supported, and multilayered rectangular plates under static loadings. While the homogeneous solutions are obtained in terms of a new and simple formalism that resemble the Stroh formalism, solutions for multilayered plates are expressed in terms of the propagator matrix. The present solutions include all the previous solutions, such as piezoelectric, piezomagnetic, purely elastic solutions, as special cases, and can therefore serve as benchmarks to check various thick plate theories and num

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29

Taylor, T. W., and A. H. Nayfeh. "Damping Characteristics of Laminated Thick Plates." Journal of Applied Mechanics 64, no. 1 (1997): 132–38. http://dx.doi.org/10.1115/1.2787263.

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We develop the analysis for the exact three-dimensional viscoelastic solution for simply supported, thick multilayered composite plate strips. Each layer is assumed to possess monoclinic or higher material symmetry and to be perfectly bonded to adjacent layers. The damping capacity, or loss factor, of the composite plate is derived using energy principles, allowing analysis of arbitrary through-the-thickness geometry for the composite plate. The damping characteristics of the composite plate, as well as its natural modes of vibration, are obtained with the aid of the matrix transfer technique.

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Gherlone, Marco, and Marco Di Sciuva. "Dynamic Behaviour of Undamaged and Damaged Multilayered Composite Plates." Key Engineering Materials 347 (September 2007): 531–36. http://dx.doi.org/10.4028/www.scientific.net/kem.347.531.

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The article deals with the application of a higher-order FEM approach to the analysis of the dynamic behaviour of undamaged and damaged multilayered composite plates. Some numerical examples show the accuracy of the developed plate mixed finite element, in terms of vibration frequencies and mode shapes, for different boundary conditions and with different damage geometries.

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31

Noor, Ahmed K., and W. Scott Burton. "Stress and free vibration analyses of multilayered composite plates." Composite Structures 11, no. 3 (1989): 183–204. http://dx.doi.org/10.1016/0263-8223(89)90058-5.

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32

Zhang, Zan, C. Feng, and K. M. Liew. "Three-dimensional vibration analysis of multilayered piezoelectric composite plates." International Journal of Engineering Science 44, no. 7 (2006): 397–408. http://dx.doi.org/10.1016/j.ijengsci.2006.02.002.

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Muc, A., and A. Ulatowska. "Local fibre reinforcement of holes in composite multilayered plates." Composite Structures 94, no. 4 (2012): 1413–19. http://dx.doi.org/10.1016/j.compstruct.2011.11.017.

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Maghsoodi, Ameneh, Abdolreza Ohadi, and Mojtaba Sadighi. "Calculation of Wave Dispersion Curves in Multilayered Composite-Metal Plates." Shock and Vibration 2014 (2014): 1–6. http://dx.doi.org/10.1155/2014/410514.

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The major purpose of this paper is the development of wave dispersion curves calculation in multilayered composite-metal plates. At first, equations of motion and characteristic equations for the free waves on a single-layered orthotropic plate are presented. Since direction of wave propagation in composite materials is effective on equations of motion and dispersion curves, two different cases are considered: propagation of wave along an axis of material symmetry and along off-axes of material symmetry. Then, presented equations are extended for a multilayered orthotropic composite-metal plat

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35

Zak, A. J., M. P. Cartmell, and W. Ostachowicz. "Dynamics of Multilayered Composite Plates With Shape Memory Alloy Wires." Journal of Applied Mechanics 70, no. 3 (2003): 313–27. http://dx.doi.org/10.1115/1.1546263.

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In this paper certain aspects of the dynamic behavior of a multilayered, composite plate with shape memory alloys (SMA) wires have been investigated. The influence of parameters such as the orientation and location of SMA wires, the orientation and relative volume fraction of reinforcing fibers, the thickness-to-length and length-to-width ratios, and different boundary conditions, on changes in the critical load, the natural frequencies and the modes of vibrations of the plate have all been studied and discussed in the paper. The use of two different techniques, generally known in the literatu

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36

Kim, M., and Y. F. Hwang. "Some structural acoustic features of multilayer composite plates." Journal of the Acoustical Society of America 94, no. 3 (1993): 1838. http://dx.doi.org/10.1121/1.407744.

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Teregulov, I. G., and E. S. Sibgatullin. "Failure criteria for multilayer composite plates and shells." Mechanics of Composite Materials 26, no. 1 (1990): 64–70. http://dx.doi.org/10.1007/bf00619422.

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Kolesnik, S. A. "Nonsteady Heat Transfer in Multilayer Anisotropic Composite Plates." Russian Engineering Research 45, no. 4 (2025): 530–34. https://doi.org/10.3103/s1068798x25700376.

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Abbaslou, A., and MR Maheri. "Prediction of the damping properties of fiber-reinforced polymer composite panels with arbitrary geometries." Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science 232, no. 2 (2016): 275–83. http://dx.doi.org/10.1177/0954406216676506.

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In this work, the modal damping of multilayered, fiber-reinforced polymer composite laminates with an arbitrary geometry have been computed using a mixed finite element-meshless method. The meshless node distribution scheme is used in conjunction with the Lagrangian quadrilateral interpolating functions to ensure the continuity of interelemental displacements. Furthermore, since the distribution of the elements is not confined to the geometry of the problem, any arbitrary geometry can be readily analyzed by using the same node and element distributions. Using the classical plate theory, togeth

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40

Kacan, Yelda O., and Faruk Elaldi. "Ballistic performance of unidirectionally oriented carbon fiber reinforced composite armor with high-velocity impact." Journal of Reinforced Plastics and Composites 39, no. 19-20 (2020): 733–41. http://dx.doi.org/10.1177/0731684420929084.

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For the last few decades, composite materials have been more popular than other conventional metal materials in the aircraft industry. Having better mechanical properties (strength, fatigue life, impact strength, corrosion resistance, etc.) and being lighter than conventional engineering materials, composites have become very important in defense industry as well. In spite of the fact that some of the composite materials such as aramid-based composites have been effectively used in body protection, they have not been so successful in heavy armored vehicles which are generally equipped with dif

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41

Chen, Jie, Ruofan Han, Dekun Liu, and Wei Zhang. "Active Flutter Suppression and Aeroelastic Response of Functionally Graded Multilayer Graphene Nanoplatelet Reinforced Plates with Piezoelectric Patch." Applied Sciences 12, no. 3 (2022): 1244. http://dx.doi.org/10.3390/app12031244.

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This paper investigates the aeroelastic flutter and vibration reduction of functionally graded (FG) multilayer graphene nanoplatelets (GPLs) reinforced composite plates with piezoelectric patch subjected to supersonic flow. Activated by the control voltage, the piezoelectric patch can generate the active mass and active stiffness that can accordingly increase the base plate’s stiffness and mass. As a result, it changes the GPLs reinforced plate’s dynamic characteristics. The motion equation of the plate-piezoelectric system is derived through the Hamilton principle. Based on the modified Halpi

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Durbaca, Ion, Nicoleta Sporea, and Ovidiu Vasile. "Assessment of the Acoustic Absorption Characteristics of Layered Composite Structures Obtained from Plates with Lignocellulosic Coatings (I)." Materiale Plastice 57, no. 2 (2019): 8–14. http://dx.doi.org/10.37358/mp.20.2.5345.

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Abstract.The paper aims to present research on the determination of the coefficient of acoustic absorption as a function of frequency, for composite monolayer plates (made of: MDF - wooden dried agglomerated fibres with medium density, RWB - rebated wood from dried beech, PS - extruded polystyrene) and multilayer (with outer coatings of: MDF, RWB and polymeric core of extruded polystyrene). The sound-absorbing behavior of such plates is highlighted in the cabins made of multilayer structures.

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Pasupuleti, Kirti, Kevin Vattappara, Sylvester Gomes, and Parvati Ramaswamy. "Thermal fatigue characteristics of 8Y2O3-ZrO2, La2Zr2O7, La2(Zr0.7Ce0.3)2O7 and La2Ce2O7 thermal barrier coatings in duplex, multilayer functionally graded and multilayer configurations." Processing and Application of Ceramics 17, no. 3 (2023): 236–47. http://dx.doi.org/10.2298/pac2303236p.

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La2Zr2O7, La2(Zr0.7Ce0.3)2O7 and La2Ce2O7 pyrochlore plasma sprayable powders were synthesized and plasma spray coated on steel plates with NiCrAlY bond coat. Three different configurations were used: duplex, multilayer functionally graded and multilayer, with different combinations of commercial 8% yttria stabilized zirconia (8YSZ) and NiCrAlY (bond coat) layers. The prepared coatings were compared with the standard duplex 8YSZ thermal barrier coatings (TBCs) with a goal to study their suitability to serve as TBCs. TBCs? layer thicknesses and interfaces were studied via SEM on polished cross

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Nayak, A. K., S. S. J. Moy, and R. A. Shenoi. "Quadrilateral finite elements for multilayer sandwich plates." Journal of Strain Analysis for Engineering Design 38, no. 5 (2003): 377–92. http://dx.doi.org/10.1243/03093240360713441.

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The bending behaviour of isotropic and laminated composite and sandwich plates has been analysed using two new C° assumed strain quadrilateral finite element formulations based on a refined form of Reddy's higher-order theory. The assumed strain approach ensures that there are no parasitic spurious zero energy modes and no shear locking. The element performances are evaluated on some standard plate tests involving closed-form solutions and experimental results. All results indicate that the present elements have satisfactory convergence properties, accuracy in the results and freedom from any

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Noor, A. K., and W. S. Burton. "Steady-state heat conduction in multilayered composite plates and shells." Computers & Structures 39, no. 1-2 (1991): 185–93. http://dx.doi.org/10.1016/0045-7949(91)90086-2.

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Moleiro, F., A. L. Araújo, and J. N. Reddy. "Benchmark exact free vibration solutions for multilayered piezoelectric composite plates." Composite Structures 182 (December 2017): 598–605. http://dx.doi.org/10.1016/j.compstruct.2017.09.035.

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Cheng, Zhen-qiang, A. K. Jemah, and F. W. Williams. "Theory for Multilayered Anisotropic Plates With Weakened Interfaces." Journal of Applied Mechanics 63, no. 4 (1996): 1019–26. http://dx.doi.org/10.1115/1.2787221.

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Rigorous kinematical analysis offers a general representation of displacement variation through thickness of multilayered plates, which allows discontinuous distribution of displacements across each interface of adjacent layers so as to provide the possibility of incorporating effects of interfacial imperfection. A spring-layer model, which has recently been used efficiently in the field of micromechanics of composites, is introduced to model imperfectly bonded interfaces of multilayered plates. A linear theory underlying dynamic response of multilayered anisotropic plates with nonuniformly we

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Dimitrienko, Yu I., and D. O. Yakovlev. "THE ASYMPTOTIC THEORY OF THERMOELASTICITY OF MULTILAYER COMPOSITE PLATES." Composites: Mechanics, Computations, Applications: An International Journal 6, no. 1 (2015): 13–51. http://dx.doi.org/10.1615/compmechcomputapplintj.v6.i1.20.

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Bokhoeva, L. A., V. E. Rogov, E. B. Bochektueva, A. B. Baldanov, and R. P. Ivanov. "Development of armored products made from multilayer composite plates." Nanotechnologies in Construction A Scientific Internet-Journal 17, no. 2 (2025): 201–9. https://doi.org/10.15828/2075-8545-2025-17-2-201-209.

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Das, Malay Kumar, Jiaqian Qin, and Priya Karn. "Effect of diamond particles on the microstructure and composition of pulse plated multilayer Ni-W/diamond composite coatings." MATEC Web of Conferences 277 (2019): 03002. http://dx.doi.org/10.1051/matecconf/201927703002.

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The research encompasses the fabrication of multilayer Ni-Wdiamond composite deposits by pulse current electrodeposition. The mean surface diameter of the diamond used for the research was 0.9 microns. The composites were fabricated under various conditions and characterized by means of SEM, EDS and XRD to investigate and analyze their microstructure, grain size and elemental distribution along with variations in morphology under different conditions. The effect of variations in forward and reverse current density along with duty cycle and the combination of various aforesaid conditions on the

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