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Relevant bibliographies by topics / Composite Plates

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Academic literature on the topic 'Composite Plates'

Author: Grafiati

Published: 4 June 2021

Last updated: 25 July 2025

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Journal articles on the topic "Composite Plates"

1

Khandan, Rasoul, Philip Sewell, Siamak Noroozi, and Mohammad Reza Ramazani. "FE Design Tool for Laminated Composite Plates." Applied Mechanics and Materials 248 (December 2012): 379–83. http://dx.doi.org/10.4028/www.scientific.net/amm.248.379.

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Considering the non-linearity, complexity and anisotropy of constitutive equations in composite materials, numerical methods are essential to evaluate the behaviour of this material. The finite element method (FEM) is a powerful computational technique for the solution of differential and integral equations that arise in various fields of engineering and applied science such as composite materials. Here, an FEM tool is designed to analyse non-linearity in the behaviour of composites caused by the effect of transverse shear and twist in laminated composite plates. The tool is established by usi

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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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Gautam, Rajeev K., and Kamal K. Kar. "Synthesis and Properties of Highly Conducting Natural Flake Graphite/Phenolic Resin Composite Bipolar Plates for Pem Fuel Cells." Advanced Composites Letters 25, no. 4 (2016): 096369351602500. http://dx.doi.org/10.1177/096369351602500402.

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Electrically conductive composite bipolar plates consisting of resole-typed phenol formaldehyde resin and natural flake graphite (NFG) have been fabricated by compression molding technique at room temperature. The aim of this study is to investigate the effects of NFG content, molding pressure, and nano-sized carbon black (NCB) on the properties of composite bipolar plates. The NFG/resin composite plates have been studied for various properties including electrical, mechanical, and thermal properties. It has been observed that the composite plates prepared at NFG content of 45 wt%, NCB content

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Veerappan, Balasubramani, Sudharshan Vasudevan, and B. Karthikeyan. "Numerical Deflection Analysis of Rectangular Laminated Composite Plates - Truck Bed - Case Study." Materials Science Forum 1070 (October 13, 2022): 71–87. http://dx.doi.org/10.4028/p-o2qaka.

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Transport industry plays a vital role in development of economy of countries. To increase the load carrying capacity of the truck, the weight of truck bed may be reduced using fibre reinforced composite material. In this work, a numerical investigation is performed to reduce the weight of the truck bed using different types of laminated composites. An extensive study is conducted using unidirectional and woven fibres of glass, carbon and Kevlar fibres with polyester, epoxy and vinyl ester resins. Carbon fibre laminated plates have higher stiffness than Glass and Kevlar composite plates. Asymme

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Pasnur, Pallavi K., and ,. Anant V. Kharche. "A Review Paper on Laminated Composite Plates." Journal of Advances and Scholarly Researches in Allied Education 15, no. 2 (2018): 612–16. http://dx.doi.org/10.29070/15/56936.

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Kanasogi, R. M., and M. C. Ray. "Active Constrained Layer Damping of Smart Skew Laminated Composite Plates Using 1–3 Piezoelectric Composites." Journal of Composites 2013 (June 5, 2013): 1–17. http://dx.doi.org/10.1155/2013/824163.

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This paper deals with the analysis of active constrained layer damping (ACLD) of smart skew laminated composite plates. The constraining layer of the ACLD treatment is composed of the vertically/obliquely reinforced 1–3 piezoelectric composites (PZCs). A finite element model has been developed for accomplishing the task of the active constrained layer damping of skew laminated symmetric and antisymmetric cross-ply and antisymmetric angle-ply composite plates integrated with the patches of such ACLD treatment. Both in-plane and out-of-plane actuations by the constraining layer of the ACLD treat

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Hadi, Nabil Hassan, and Basim Jameel Hamood. "Vibration Analysis of a Composite Plate with Delamination." Journal of Engineering 21, no. 2 (2015): 144–64. http://dx.doi.org/10.31026/j.eng.2015.02.09.

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The use of composite materials has vastly increased in recent years. Great interest is therefore developed in the damage detection of composites using non- destructive test methods. Several approaches have been applied to obtain information about the existence and location of the faults. This paper used the vibration response of a composite plate to detect and localize delamination defect based on the modal analysis. Experiments are conducted to validate the developed model. A two-dimensional finite element model for multi-layered composites with internal delamination is established. FEM progr

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Srinivas, K. R. "Experimental Investigation of Mechanical Properties for Tamarind Shell Particles as Filler in Epoxy Composite." International Journal of Engineering Research and Advanced Technology (IJERAT) 3, no. 3 (2017): 40–49. https://doi.org/10.5281/zenodo.439655.

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<em>This paper explores the potential of tamarind shell particles as a filler in epoxy composites. The tamarind shell particles reinforced epoxy composites plates were prepared by varying both tamarind shell particle and epoxy volume percentage. The mechanical properties such as tensile strength, deflection, impact, hardness and specific gravity are evaluated for different composition of composite plates.This paper explores the potential of tamarind shell particles as a filler in epoxy composites. The tamarind shell particles reinforced epoxy composites plates were prepared by varying both tam

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Sirajudeen, Rahima Shabeen, and Alagusundaramoorthy P. "GFRP Stiffened Plate with Square Cutout under Axial and Out-of-Plane Load." Polymers 13, no. 8 (2021): 1185. http://dx.doi.org/10.3390/polym13081185.

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The high-strength-to-weight ratio and corrosion resistance properties of glass-fiber-reinforced polymer (GFRP) composites makes them potentially well-suited for application in ship structures, bridges and off-shore oil platforms. These structures are often formed by stiffened plates and are subjected to axial load and out-of-plane load. Cutouts and openings are provided in the plates for access and maintenance. The main objective of this study was to examine the buckling behavior of GFRP-stiffened composite plates with square cutouts under a combination of axial and out-of-plane load up to fai

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Chen, Hui, Xiao-Hong Xia, Li Yang, Yue-de He, and Hong-bo Liu. "Preparation and characterization of graphite/resin composite bipolar plates for polymer electrolyte membrane fuel cells." Science and Engineering of Composite Materials 23, no. 1 (2016): 21–28. http://dx.doi.org/10.1515/secm-2013-0306.

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AbstractPreparing conductive composite bipolar plates for fuel cells by compression molding is a promising research direction. The very key point is how to choose the conductivity filler and binder to meet the requirement. In this article, natural graphite and expanded graphite were used as the filler, and phenolic resin and epoxy resin were used as the binder. The composite bipolar plates were prepared by solution intercalation mixing, compression molding, and curing. The variations in electrical conductivity and mechanical properties were evaluated with the resin content. The results show th

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Dissertations / Theses on the topic "Composite Plates"

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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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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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Lazarus, Kenneth B. "Induced strain actuation of composite plates." Thesis, Massachusetts Institute of Technology, 1989. http://hdl.handle.net/1721.1/41235.

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Souza, Carlos Eduardo de. "Nonlinear aeroelasticity of composite flat plates." Instituto Tecnológico de Aeronáutica, 2012. http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2243.

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This work presents a study on aeroelastic analyses of composite laminated flat plates subject to large displacements through the coupling of a nonlinear corotational shell finite element (FE) with an unsteady vortex-lattice method (UVLM) formulation. A FE implemented for the analysis of flat plates has been extended to model laminated composites with different lamina orientations. An UVLM formulation that is capable of coupling with this large displacement structural model is implemented. An explicit partitioned method is evaluated for the coupling of both models, using spline functions to in

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Simelane, Philemon Sphiwe. "Thermal buckling of laminated composite plates." Thesis, Peninsula Technikon, 1998. http://hdl.handle.net/20.500.11838/1240.

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Thesis (MTech (Mechanical Engineering))--Peninsula Technikon, 1998<br>However, studies were also conducted for the buckling of composite laminates involving temperature distribution. Chen and Chen (1991) studied thermal buckling of laminated plates under uniform and nonuniform temperature distribution using the eight-node Serendipity finite element. Mathew, Singh and Rao (1992) investigated thermal buckling of antisymmetric cross-ply composite laminates with a onedimensional furite element having two nodes and six degrees of freedom. Chandrashekhara (1992) accounted for transverse shear

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Tiwari, Nachiketa. "Secondary Buckling of Laminated Composite Plates." Diss., Virginia Tech, 1999. http://hdl.handle.net/10919/37789.

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The postbuckling load carrying capacity of composite plates offers immense potential to their applications for loads exceeding their primary buckling load. However, such an efficient and economical usage of these plates can be reliable only if the nonlinear postbuckling behavior of these plates, which includes a good understanding of secondary buckling, is understood thoroughly. The present investigation is an attempt to understand secondary buckling of almost square composite clamped-simply supported plates, both unstiffened as well as stiffened, in some detail. With the help of the finite e

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Moorthy, Jayashree. "Dynamic instability of composite laminated plates." Thesis, Virginia Polytechnic Institute and State University, 1989. http://hdl.handle.net/10919/52090.

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Dynamic instability in a laminated composite plate is studied using the finite element technique. The governing equations are derived based on the first order shear deformation theory with a linear strain-displacement relationship. The regions of instability for the resulting set of coupled Mathieu equations are obtained using a method of simultaneous diagonalization. Boundary frequencies generated using a first subdeterminant approximation to the infinite determinant are compared with those obtained by using the more accurate second subdeterminant as well as with frequencies from an analytica

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Olsson, Robin. "Impact response and delamination of composite plates /." Stockholm, 1998. http://www.lib.kth.se/abs98/olss0528.pdf.

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Tippetts, Trevor 1977. "Modeling impact damage in laminated composite plates." Thesis, Massachusetts Institute of Technology, 2003. http://hdl.handle.net/1721.1/82782.

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Abdelnaser, Ahmad Shehadeh. "Random vibrations of composite beams and plates." Diss., Virginia Tech, 1992. http://hdl.handle.net/10919/37691.

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The response characteristics of beams and plates made from composite laminates are strongly affected by the shear deformations of their layers. However, incorporation of the shear deformation further complicates the equations of motion and their analysis. As a result the vibration analysis of such structures have been limited to simple free vibration studies such as determination of their frequencies. The forced vibration problems of these structures have been solved by exact methods for only some very simple cases. In this study, a generalized modal approach is presented to solve more general

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Books on the topic "Composite Plates"

1

Ye, Jianqiao. Laminated Composite Plates and Shells. Springer London, 2003. http://dx.doi.org/10.1007/978-1-4471-0095-9.

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2

J, Turvey G., and Marshall I. H, eds. Buckling and postbuckling of composite plates. Chapman & Hall, 1995.

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Dong, S. B. Edge vibrations in laminated composite plates. American Society of Mechanical Engineers, 1985.

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Turvey, G. J., and I. H. Marshall, eds. Buckling and Postbuckling of Composite Plates. Springer Netherlands, 1995. http://dx.doi.org/10.1007/978-94-011-1228-4.

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S, Springer George, and United States. National Aeronautics and Space Administration., eds. Compression behavior of delaminated composite plates. Department of Aeronautics and Astronautics, Stanford University, 1989.

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Hussein, Raafat M. M. Composite panels/plates: Analysis and design. Technomic Pub., 1986.

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George C. Marshall Space Flight Center, ed. Basic mechanics of laminated composite plates. Marshall Space Flight Center, National Aeronautics and Space Administration, 1994.

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Turvey, G. J. Buckling and Postbuckling of Composite Plates. Springer Netherlands, 1995.

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9

Finn, Scott R. Composite plates impact damage: An atlas. Technomic Pub. Co., 1991.

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Nettles, A. T. Basic mechanics of laminated composite plates. National Aeronautics andSpace Administration, 1994.

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Book chapters on the topic "Composite Plates"

1

Oñate, Eugenio. "Composite Laminated Plates." In Structural Analysis with the Finite Element Method Linear Statics. Springer Netherlands, 2013. http://dx.doi.org/10.1007/978-1-4020-8743-1_7.

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Hwu, Chyanbin. "Laminated Composite Plates." In Mechanics of Laminated Composite Structures. CRC Press, 2024. http://dx.doi.org/10.1201/9781003470465-3.

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Gay, Daniel. "Transverse Shear Behavior of Multilayered Plates." In Composite Materials, 4th ed. CRC Press, 2022. http://dx.doi.org/10.1201/9781003195788-21.

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Gay, Daniel. "Mechanical Behavior of Thin Laminated Plates." In Composite Materials, 4th ed. CRC Press, 2022. http://dx.doi.org/10.1201/9781003195788-14.

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Birman, Victor. "Mechanics of Composite Plates." In Plate Structures. Springer Netherlands, 2010. http://dx.doi.org/10.1007/978-94-007-1715-2_5.

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Gdoutos, E. E. "Crack Growth in Duplex Plates." In Composite Structures 3. Springer Netherlands, 1985. http://dx.doi.org/10.1007/978-94-009-4952-2_42.

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GangaRao, Hota V. S., and Woraphot Prachasaree. "Analysis of FRP Composite Plates." In FRP Composite Structures. CRC Press, 2021. http://dx.doi.org/10.1201/9781003196754-6.

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Si-Wei, Cai, and Cai Min. "A Refined Theory for Laminated Anisotropic Plates." In Composite Structures. Springer Netherlands, 1991. http://dx.doi.org/10.1007/978-94-011-3662-4_30.

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Bhaskar, K., T. K. Varadan, and S. Savithri. "Analysis of Thick Laminated Shells and Plates." In Composite Structures. Springer Berlin Heidelberg, 1992. http://dx.doi.org/10.1007/978-3-662-11345-5_17.

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Altenbach, Holm, Johannes Altenbach, and Wolfgang Kissing. "Differential Operators for Rectangular Plates (Classical Plate Theory)." In Mechanics of Composite Structural Elements. Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-662-08589-9_14.

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Conference papers on the topic "Composite Plates"

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Franke, Florian, Sebastian Heimbs, Christian Seidel, Patrik-Vincent Brudzinski, Dominic Huehn, and Uli Burger. "High Speed Impact Testing of Thermoplastic Composite Plates." In Vertical Flight Society 73rd Annual Forum & Technology Display. The Vertical Flight Society, 2017. http://dx.doi.org/10.4050/f-0073-2017-12166.

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This paper presents the methodology and results for ballistic impact testing of thermoplastic composite materials. Ten different materials are investigated. The impact behavior of Aluminum 6082 is used as a reference to compare the results. The impact tests are performed with a gas cannon. Force - time, displacement - time as well as velocity data are recorded. Analytic suggestions for the calculation of the penetration speed of the materials are compared with measured results. It can be seen that it is possible to calculate the penetration speed within a certain percentage of the measured val

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Quintelier, Jan, Pieter Samyn, Patrick De Baets, Danny Van Hemelrijck, and Joris Degrieck. "WEAR MECHANISMS OF PULTRUDED GFR COMPOSITE PLATES." In 60º Congresso Anual da ABM. Editora Blucher, 2005. https://doi.org/10.5151/2594-5327-2005-13668-0362.

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Yang, Wenbin, puhong tang, and jiabo zhang. "Electrical conductivity study of graphite composite bipolar plates." In Seventh International Conference on Advanced Electronic Materials, Computers, and Software Engineering (AEMCSE 2024), edited by Lvqing Yang. SPIE, 2024. http://dx.doi.org/10.1117/12.3038141.

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Auad, Samir P., Jamires S. C. Praciano, Elias S. Barroso, João B. M. Sousa Jr., and Evandro Parente Jr. "Isogeometric analysis of fgm plates." In Brazilian Conference on Composite Materials. Pontifícia Universidade Católica do Rio de Janeiro, 2018. http://dx.doi.org/10.21452/bccm4.2018.16.09.

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Sorohan, Stefan, Ioan Parausanu, Adrian Motomancea, and Dumitru I. Caruntu. "Dynamic Analysis of Composite Plates." In ASME 2005 International Mechanical Engineering Congress and Exposition. ASMEDC, 2005. http://dx.doi.org/10.1115/imece2005-82252.

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The paper presents comparatively the measured and estimated natural frequencies and mode shapes of a rectangular orthotropic panel. The experimental tests were performed using a shaker. The plate was fixed in horizontal position directly on the shaker armature using a rigid rod. The experimental modes shapes were visualized using sand particles. The measured natural frequencies and also the modes shapes correspond to the whole system in motion. So, the analytic model of the plate must include the effect of the vibrator connected to the plates. The purpose of this experimental measurements and

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Chen, J. K., and J. E. Beraun. "Three-Dimensional Penetration Modelling of Composite Plates." In ASME 1996 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 1996. http://dx.doi.org/10.1115/imece1996-0606.

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Abstract The smoothed particle hydrodynamics (SPH) technique in conjunction with the macro-mechanics approach for fiber composites was developed to predict impact damage of composite structures. For investigating the detailed perforation process and damage progression, 3-D simulations of a graphite/epoxy composite laminate struck by a steel projectile were performed. The predicted damage in the composite target agrees well qualitatively with the experimental results. This study has demonstrated that SPH can be a robust and viable analytical tool for predicting the accurate response of fiber-re

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Jia, Hongyu, and Craig A. Rogers. "The Effect of Toughened Composites on the Static Buckling Load and Buckled Position of Composite Laminated Plates." In ASME 1997 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 1997. http://dx.doi.org/10.1115/imece1997-1038.

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Abstract A nonlinear analysis of the buckling and post-buckling responses of a simply supported laminated composite plate under an axial in-plane compressive load is presented. The model for symmetric cross-ply laminated composite plates made from various composite materials, such as, Graphite/Epoxy, Graphite/PEKK, Graphite/PEEK, and Kevlar/PEKK is given here. The governing equations of post-buckling composite plates with large strains are obtained by using the minimum total potential energy principle. The post-buckling behaviors of Graphite/Epoxy composite plate and toughened composite plates

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Jia, Hongyu, and Craig A. Rogers. "The Effect of Toughened Composites on Dynamic Behaviors of Composite Laminates Under the In-Plane Dynamic Load." In ASME 1997 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 1997. http://dx.doi.org/10.1115/imece1997-1053.

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Abstract In order to investigate the effect of toughened composites on the dynamic behavior of the laminated composite plates under in-plane loading, a simply supported laminated composite plate under the axial in-plane dynamic load is studied. A model for symmetric cross-ply laminated composite plate is presented here. The gorvening equations of motion are obtained by using Lagrange equations. The laminated composite plates are made from various composite materials, such as, Graphite/Epoxy, Graphite/PEKK, Graphite/PEEK, and Kevlar/PEKK. This model considers the large strain, transverse inerti

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Ari-Gur, Judah, and Samuel Simonetta. "Pulse buckling of composite plates." In 35th Structures, Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics, 1994. http://dx.doi.org/10.2514/6.1994-1435.

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Aygun, A. "SOUND RADIATION FROM COMPOSITE PLATES." In ACOUSTICS 2021. Institute of Acoustics, 2021. http://dx.doi.org/10.25144/13765.

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Reports on the topic "Composite Plates"

1

Nayfeh, Adnan H. Interaction of Ultrasonic Waves with Composite Plates. Defense Technical Information Center, 1987. http://dx.doi.org/10.21236/ada191879.

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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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Trinh, K. V. Modeling the in-plane tension failure of composite plates. Office of Scientific and Technical Information (OSTI), 1997. http://dx.doi.org/10.2172/563207.

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Reddy, J. N. A Refined Nonlinear Analysis of Laminated Composite Plates and Shells. Defense Technical Information Center, 1987. http://dx.doi.org/10.21236/ada184436.

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Jha, Ratneshwar. Wavelet Spectral Finite Elements for Wave Propagation in Composite Plates. Defense Technical Information Center, 2012. http://dx.doi.org/10.21236/ada565193.

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Norgard, John D., Randall Mussellman, Michael C. Wicks, et al. Modeling of Composite Scenes Using Wires, Plates and Dielectric Parallelized (WIPL-DP). Defense Technical Information Center, 2006. http://dx.doi.org/10.21236/ada455065.

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Steinzig, Michael, and Filipe Broetto. Residual Stress measurements in thin composite plates using the hole drilling technique. Office of Scientific and Technical Information (OSTI), 2014. http://dx.doi.org/10.2172/1159052.

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Thornell, Travis, Charles Weiss, Sarah Williams, et al. Magnetorheological composite materials (MRCMs) for instant and adaptable structural control. Engineer Research and Development Center (U.S.), 2020. http://dx.doi.org/10.21079/11681/38721.

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Magnetic responsive materials can be used in a variety of applications. For structural applications, the ability to create tunable moduli from relatively soft materials with applied electromagnetic stimuli can be advantageous for light-weight protection. This study investigated magnetorheological composite materials involving carbonyl iron particles (CIP) embedded into two different systems. The first material system was a model cementitious system of CIP and kaolinite clay dispersed in mineral oil. The magnetorheological behaviors were investigated by using parallel plates with an attached ma

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Colonna, Martino, Lorenzo Crosetta, Alessandro Nanni, Daniel Colombo, and Tommaso Maria Brugo. Carbon composite plates for running shoes: a novel testing method for the measure of flexural stiffness, rebound and damping. Purdue University, 2022. http://dx.doi.org/10.5703/1288284317544.

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Alexander, Chris. L52318 State of the Art Assessment of Composite Repair Systems. Pipeline Research Council International, Inc. (PRCI), 2010. http://dx.doi.org/10.55274/r0000005.

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Composite materials have been used to repair high pressure transmission pipelines. Over this time period a wide variety of composite systems have been developed and evaluated. With the increased demands being placed on pipeline systems around the world, it is expected that the market potential for composite repair systems will continue to expand. Additionally, as composite technology is further developed the opportunities for new applications will expand. An assessment of this composite repair technology is needed. This report has been developed to provide industry with a state of the art asse

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