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Relevant bibliographies by topics / Laminated and sandwich composite

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Academic literature on the topic 'Laminated and sandwich composite'

Author: Grafiati

Published: 14 March 2023

Last updated: 31 July 2025

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Journal articles on the topic "Laminated and sandwich composite"

1

Sebaey, TA, and Ahmed Wagih. "Flexural properties of notched carbon–aramid hybrid composite laminates." Journal of Composite Materials 53, no. 28-30 (2019): 4137–48. http://dx.doi.org/10.1177/0021998319855773.

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Hybrid composite laminates are currently receiving researchers’ attention due to their specific advantages in designing laminates with improved specific strength and stiffness. One of the main disadvantages of polymeric laminated composites is their high sensitivity to notches, which cannot be avoided in design. This paper presents a comparison between two common hybridization techniques, namely sandwich and intra-ply hybridization. The study adopts experimental observations to investigate the influence of hybridization method on the flexural properties of notched carbon–aramid hybrid laminate

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Arsalan, Hussain Khan, and Misbah Danish Mr. "FINITE ELEMENT ANALYSIS OF LAMINATED SANDWICH STRUCTURE." International Journal of Advances in Engineering & Scientific Research 5, no. 3 (2018): 14–33. https://doi.org/10.5281/zenodo.10780792.

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<strong>ABSTRACT</strong> <em>In modern civil engineering structures, laminated composites are widely used in various applications including roof of buildings, bridge decks, structural panels and beams. Using the laminated composite material in construction introduces many advantages such as high strength/stiffness to weight ratio, survivability in extreme weather conditions, durability, fatigue resistance, and design flexibility, easy to install in structure replacement. The behavior of laminated composites under free vibration, bending and buckling mode is very complex phenomenon because man

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Çınar, Okan, Merve Erdal, and Altan Kayran. "Accurate equivalent models of sandwich laminates with honeycomb core and composite face sheets via optimization involving modal behavior." Journal of Sandwich Structures & Materials 19, no. 2 (2016): 139–66. http://dx.doi.org/10.1177/1099636215613934.

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An approach is introduced for determining accurate two-dimensional equivalent laminated models of sandwich laminates with honeycomb core and composite facesheets by optimization involving modal behavior. The approach relies on minimizing the objective function which is defined as the sum of the square of the differences between the natural frequencies of the honeycomb sandwich laminate estimated by the finite element analysis of the 3D detailed model with the actual honeycomb core geometry and by the 2D equivalent laminated model with the honeycomb core replaced by the equivalent 2D orthotropi

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Zhu, Xiujie, Chao Xiong, Junhui Yin, Dejun Yin, and Huiyong Deng. "Bending Experiment and Mechanical Properties Analysis of Composite Sandwich Laminated Box Beams." Materials 12, no. 18 (2019): 2959. http://dx.doi.org/10.3390/ma12182959.

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The failure modes, ultimate load, stiffness performance, and their influencing factors of a composite sandwich laminated box beam under three-point bending load are studied by an experiment, finite element model, and analytical method. The three-point bending experiment was carried out on three different core composite sandwich laminated box beams, and the failure modes and bearing capacity were studied. With the use of composite progressive damage analysis and the core elastoplastic constitutive model, the finite element model of the composite sandwich laminated box beam was established, and

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Lu, Ping, Xu Dong Liu, Xue Qiang Ma, and Wei Bo Huang. "Analysis of Damping Characteristics for Sandwich Beams with a Polyurea Viscoelastic Layer." Advanced Materials Research 374-377 (October 2011): 764–69. http://dx.doi.org/10.4028/www.scientific.net/amr.374-377.764.

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Constrained layer damping treatments such as sandwich beams are considered as the most efficient way of introducing vibration damping into a structure. The dynamic mechanical properties and damping behavior of a laminated sandwich composite beam inserted with a viscoelastic layer is investigated. A quantitative analysis of damping in the sandwich laminated composite beam has been conducted through the theoretical and experimental method. Traditional epoxy and new kind of polyurea viscoelastic layer are selected to analyze the damping properties. Results showed that the polyurea viscoelastic la

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Hami, B., A. Irekti, C. Aribi, B. Bezzazi, and A. Mir. "Experimental Study of Sandwich Multilayer Reinforced by Glass Fibre and Agglomerated Cork." Advanced Composites Letters 23, no. 5 (2014): 096369351402300. http://dx.doi.org/10.1177/096369351402300503.

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This paper presents an experimental study which is determined the mechanical properties of a composite material sandwich multilayer developed in the laboratory of mechanics of materials and composites, Materials Research Unit, process and environment. This type of sandwich is composed of four layers laminated based on an epoxy resin reinforced by woven glass fibres and mast between which three plates of agglomerated cork with stacked alternately laminated layers. Specimens for bending tests three and four points were prepared from the multilayer sandwich panels. A first series of static three-

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Cui, Xiao Dong, Tao Zeng, and Dai Ning Fang. "Study on Ballistic Energy Absorption of Laminated and Sandwich Composites." Key Engineering Materials 306-308 (March 2006): 739–44. http://dx.doi.org/10.4028/www.scientific.net/kem.306-308.739.

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The impact response and energy absorbing characteristics of laminated, foam sandwich and honeycomb sandwich composites under ballistic impact have been studied in this investigation. An improved model is proposed in this paper to predict the ballistic property of the laminated composites. In this model, the material structures related to fiber lamination angles are designed in terms of their anti-impacting energy absorption capability. The ballistic limit speed and energy absorption per unit thickness of the three composites under different conditions are calculated. It is shown that honeycomb

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Vemuluri, Ramesh Babu, Vasudevan Rajamohan, and Ananda Babu Arumugam. "Dynamic characterization of tapered laminated composite sandwich plates partially treated with magnetorheological elastomer." Journal of Sandwich Structures & Materials 20, no. 3 (2016): 308–50. http://dx.doi.org/10.1177/1099636216652573.

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This study investigates the dynamic performance of the partially treated magnetorheological elastomer tapered composite sandwich plates. Various partially treated tapered magnetorheological elastomer laminated composite sandwich plate models are formulated by dropping-off the plies longitudinally in top and bottom composite face layers to yield tapered plates as the face layers. The uniform rubber and magnetorheological elastomer materials are considered as the core layer. The governing differential equations of motion of the various partially treated magnetorheological elastomer tapered compo

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Bir, Amarpreet S., Hsin Piao Chen, and Hsun Hu Chen. "Optimum Stacking Sequence Design of Composite Sandwich Panel Using Genetic Algorithms." Advanced Materials Research 585 (November 2012): 29–33. http://dx.doi.org/10.4028/www.scientific.net/amr.585.29.

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In the present study, both critical buckling load maximization and face-sheet laminate thickness minimization problems for the composite sandwich panel, subjected to bi-axial compressive loading under various imposed constraints have been investigated using genetic algorithms. In the previously published work, the optimization of simple composite laminate panels with only even number of laminae has been considered [1, 3]. The present work allows the optimization of a composite sandwich panel with both even and odd number of laminae in the face-sheet laminates. Also, the effects of the bending-

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Kumar, Pavan, and CV Srinivasa. "On buckling and free vibration studies of sandwich plates and cylindrical shells: A review." Journal of Thermoplastic Composite Materials 33, no. 5 (2018): 673–724. http://dx.doi.org/10.1177/0892705718809810.

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Many review articles were published on free vibration and buckling of laminated composites, sandwich plates, and shells. The present article reviews the literature on the buckling and free vibration analysis of shear deformable isotropic and laminated composite sandwich plates and shells using various methods available for plates in the past few decades. Various theories, finite element modeling, and experimentations have been reported for the analysis of sandwich plates and shells. Few papers on functionally graded material plates, plates with smart skin (electrorheological, magnetorheologica

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Dissertations / Theses on the topic "Laminated and sandwich composite"

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Zhao, Huyue. "Stress Analysis of Tapered Sandwich Panels with Isotropic or Laminated Composite Facings." Fogler Library, University of Maine, 2002. http://www.library.umaine.edu/theses/pdf/ZhaoH2002.pdf.

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Nayak, Ajaya Kumar. "On dynamic analysis of laminated composite and sandwich plates using finite element method." Thesis, University of Southampton, 2002. https://eprints.soton.ac.uk/43633/.

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Two new multi-layered plate bending elements (DKT/CST and DKT/LST) are developed based on a combination of the three model Discrete Kirchhoff theory (DKT) triangular plate bending element, the three model constant strain triangle (CST) and the six noded linear strain triangle (LST). Both frequency independent and frequency dependent damping of viscoelastic materials are considered. An iterative complex eigensolver is used to compute the natural frequencies and model loss factors. Several bench mark problems are solved using these new multi-layer plate elements. As the plate bending elements pr

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Kilic, Yavuz S. M. Massachusetts Institute of Technology. "Impact and energy absorption of laminated and sandwich composites." Thesis, Massachusetts Institute of Technology, 2008. http://hdl.handle.net/1721.1/44883.

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Thesis (S.M. in Naval Architecture and Marine Engineering)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2008.<br>Includes bibliographical references (p. 115-131).<br>Advanced fiber reinforced composites combine high specific strength and stiffness. Advanced composites are currently being introduced into modern U.S. Navy ships to achieve weight savings, maintenance reduction, and signature reduction. These advancements manifest themselves in Naval ships as increases in survivability, payload, range, speed, and weapon systems performance. In this thesis, vinyl ester r

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Monge, J. C., J. L. Mantari, and R. A. Arciniega. "Computational semi-analytical method for the 3D elasticity bending solution of laminated composite and sandwich doubly-curved shells." Elsevier Ltd, 2020. http://hdl.handle.net/10757/656405.

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El texto completo de este trabajo no está disponible en el Repositorio Académico UPC por restricciones de la casa editorial donde ha sido publicado.<br>In this paper, a three-dimensional numerical solution for the bending study of laminated composite doubly-curved shells is presented. The partial differential equations are solved analytically by the Navier summation for the midsurface variables; this method is only valid for shells with constant curvature where boundary conditions are considered simply supported. The partial differential equations present different coefficients, which depend o

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Ghoor, Ismail B. "The response of concave singly curved fibre reinforced moulded sandwich and laminated composite panels to blast loading." Master's thesis, University of Cape Town, 2018. http://hdl.handle.net/11427/27811.

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Composite materials are increasingly being used in a wide range of structural applications. These applications range from bicycle frames and building facades to hulls of marine ships. Their popularity is due to the high specific strength and stiffness properties, corrosion resistance, and the ability to tailor their properties to a required application. With the increasing use of composites, there is a need to better understand the material and damage behaviour of these structures. In recent years, the increased frequency of wars and terror attacks have prompted investigations into composite f

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Ghinet, Sebastian. "Statistical energy analysis of the transmission loss of sandwich and laminate composite structures." Thèse, Université de Sherbrooke, 2005. http://savoirs.usherbrooke.ca/handle/11143/1770.

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The present study emerges from a present industry need for accurate and fast numerical modeling approaches to estimate the vibro-acoustic behaviours of multilayered composite and viscoelastic treatments configurations.The structure is modeled using a wave approach applied to various multilayer configurations such as: symmetrical laminate composite, symmetrical sandwich composite and general symmetrical or unsymmetrical laminate or sandwich composite as well as viscoelastic treatments. Three behavioural modeling approaches are investigated: smeared laminate, discrete layer sandwich and general

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IURLARO, LUIGI. "Development of refined models for multilayered composite and sandwich structures: analytical formulation, FEM implementation and experimental assessment." Doctoral thesis, Politecnico di Torino, 2015. http://hdl.handle.net/11583/2606162.

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Over the last three decades, composite materials have been increasingly used in different engineering field due to their high stiffness-to-weight and strength-to-weight ratios. Nowadays, relatively thick laminated composite and sandwich materials with one hundred or more layers find their applications in primary load-bearing structural components of the modern aircraft. To ensure a reliable design and failure prediction, accurate evaluation of the strain/stress state is mandatory. A high-fidelity analysis of multilayered composite and sandwich structures can be achieved by adopting detailed 3D

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Shah, Priyal. "Computational Analysis of Elastic Moduli of Covalently Functionalized Carbon Nanomaterials, Infinitesimal Elastostatic Deformations of Doubly Curved Laminated Shells, and Curing of Laminates." Diss., Virginia Tech, 2017. http://hdl.handle.net/10919/77034.

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We numerically analyze three mechanics problems described below. For each problem, the developed computational model is verified by comparing computed results for example problems with those available in the literature. Effective utilization of single wall carbon nanotubes (SWCNTs) and single layer graphene sheets (SLGSs) as reinforcements in nanocomposites requires their strong binding with the surrounding matrix. An effective technique to enhance this binding is to functionalize SWCNTs and SLGSs by covalent attachment of appropriate chemical groups. However, this damages their pristin

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Alanbay, Berkan. "Free Vibrations and Static Deformations of Composite Laminates and Sandwich Plates using Ritz Method." Diss., Virginia Tech, 2020. http://hdl.handle.net/10919/103087.

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In this study, Ritz method has been employed to analyze the following problems: free vibrations of plates with curvilinear stiffeners, the lowest 100 frequencies of thick isotropic plates, free vibrations of thick quadrilateral laminates and free vibrations and static deformations of rectangular laminates, and sandwich structures. Admissible functions in the Ritz method are chosen as a product of the classical Jacobi orthogonal polynomials and weight functions that exactly satisfy the prescribed essential boundary conditions while maintaining orthogonality of the admissible functions. For free

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Taetragool, Unchalisa. "Optimal Parameters for Doubly Curved Sandwich Shells, Composite Laminates, and Atmospheric Plasma Spray Process." Diss., Virginia Tech, 2018. http://hdl.handle.net/10919/81978.

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Optimization is a decision making process to solve problems in a number of fields including engineering mechanics. Bio-inspired optimization algorithms, including genetic algorithm (GA), have been studied for many years. There is a large literature on applying the GA to mechanics problems. However, disadvantages of the GA include the high computational cost and the inability to get the global optimal solution that can be found by using a honeybee-inspired optimization algorithm, called the New Nest-Site Selection (NeSS). We use the NeSS to find optimal parameters for three mechanics problem

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Books on the topic "Laminated and sandwich composite"

1

Center, Langley Research, ed. A higher-order bending theory for laminated composite and sandwich beams. National Aeronautics and Space Administration, Langley Research Center, 1997.

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Center, Langley Research, ed. A higher-order bending theory for laminated composite and sandwich beams. National Aeronautics and Space Administration, Langley Research Center, 1997.

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3

F, Lung S., Gupta K. K, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. A three-node C ̊element for analysis of laminated composite sandwich shells. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

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F, Lung S., Gupta K. K, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. A three-node C ̊element for analysis of laminated composite sandwich shells. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

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5

Yu, Yi-Yuan. Vibrations of Elastic Plates: Linear and Nonlinear Dynamical Modeling of Sandwiches, Laminated Composites, and Piezoelectric Layers. Springer New York, 1996.

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6

Chamis, C. C. Fiber composite sandwich thermostuctural behavior, computationalsimulation. National Aeronautics and Space Administration, 1986.

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7

Martin, C. Wayne. A three-node C(superscript)0 element for analysis of laminated composite sandwich shells. Ames Research Center, 1989.

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Center, Langley Research, ed. Analytic and computational perspectives of multi-scale theory for homogeneous, laminated composite, and sandwich beams and plates. National Aeronautics and Space Administration, Langley Research Center, 2012.

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9

Nettles, A. T. (Alan T.), Jackson J. R, and George C. Marshall Space Flight Center, eds. Comparison of open-hole compression strength and compression after impact strength on carbon fiber/epoxy laminates for the Ares I composite interstage. National Aeronautics and Space Administration, Marshall Space Flight Center, 2011.

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10

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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Book chapters on the topic "Laminated and sandwich composite"

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Hwu, Chyanbin. "Composite Sandwich Construction." In Mechanics of Laminated Composite Structures. CRC Press, 2024. http://dx.doi.org/10.1201/9781003470465-6.

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Vaidya, Uday K. "Impact Response of Laminated and Sandwich Composites." In Impact Engineering of Composite Structures. Springer Vienna, 2011. http://dx.doi.org/10.1007/978-3-7091-0523-8_4.

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Mittelstedt, Christian. "Laminate and Sandwich Beams." In Mechanics of Composite Structures. Springer Berlin Heidelberg, 2025. https://doi.org/10.1007/978-3-662-70788-3_23.

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Manalo, Allan, Thiru Aravinthan, and Warna Karunasena. "Shear Behavior of Glue-Laminated Composite Sandwich Beams." In Advances in FRP Composites in Civil Engineering. Springer Berlin Heidelberg, 2011. http://dx.doi.org/10.1007/978-3-642-17487-2_29.

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Dey, Sudip, Tanmoy Mukhopadhyay, and Sondipon Adhikari. "Uncertainty Quantification for Skewed Laminated Soft-core Sandwich Panels." In Uncertainty Quantification in Laminated Composites. CRC Press, 2018. http://dx.doi.org/10.1201/9781315155593-10.

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Kerr-Anderson, Eric, Selvum Pillay, Basir Shafiq, and Uday K. Vaidya. "Compressively Pre-stressed Navy Relevant Laminated and Sandwich Composites Subjected to Ballistic Impact." In Dynamic Failure of Composite and Sandwich Structures. Springer Netherlands, 2012. http://dx.doi.org/10.1007/978-94-007-5329-7_4.

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Altenbach, Holm, Johannes Altenbach, and Wolfgang Kissing. "Elastic Behavior of Laminate and Sandwich Composites." In Mechanics of Composite Structural Elements. Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-662-08589-9_4.

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Altenbach, Holm, Johannes Altenbach, and Wolfgang Kissing. "Elastic Behavior of Laminate and Sandwich Composites." In Mechanics of Composite Structural Elements. Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-10-8935-0_4.

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Zhu, Shengqing, and Gin Boay Chai. "Impact of Aluminum, CFRP Laminates, Fibre-Metal Laminates and Sandwich Panels." In Composite Materials and Joining Technologies for Composites, Volume 7. Springer New York, 2013. http://dx.doi.org/10.1007/978-1-4614-4553-1_21.

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Baier, H. J. "Composite Laminate and Sandwich Optimization with Applications." In Optimization of Large Structural Systems. Springer Netherlands, 1993. http://dx.doi.org/10.1007/978-94-010-9577-8_51.

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Conference papers on the topic "Laminated and sandwich composite"

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Mejdi, Abderrazak, Bryce Gardner, and Chadwyck Musser. "Comprehensive Modeling Approach for High-Frequency Structural Properties and Noise Transmission of Composite Panels." In Vertical Flight Society 71st Annual Forum & Technology Display. The Vertical Flight Society, 2015. http://dx.doi.org/10.4050/f-0071-2015-10069.

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This paper addresses the modeling of the thick uniform or general composite laminate and sandwich structures commonly used for helicopter construction to support the fast and accurate modelling of such structures for high frequencies using SEA. For laminated composites, each layer of the lamina is described by a Reissner-Mindlin displacement field leading to equilibrium relations accounting for membrane, transverse shearing, bending and full inertial terms. The sandwich model adheres to the sandwich panels' assumptions and uses a discrete displacement field for each layer, also allowing for ou

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Chiu, Lisa, Mark Robeson, Kenneth Hunziker, and Clark Andrews. "Analysis of Shockwave Tolerant Features for Small-Volume Composite Rotorcraft Structure." In Vertical Flight Society 72nd Annual Forum & Technology Display. The Vertical Flight Society, 2016. http://dx.doi.org/10.4050/f-0072-2016-11546.

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The capability for candidate shockwave tolerant features to contribute to shockwave attenuation and residual structural integrity of small-volume rotorcraft structures was evaluated in this study. To first understand the shockwave reflection and transmission effects of an explosive event on small-volume enclosed geometry, Finite Element Analysis (FEA) was performed to assess the relationship between the enclosed volume and explosive energy. The FEA techniques included a fluid dynamics based Arbitrary Lagrangian Eulerian (ALE) method as well as an empirically based method. With an understanding

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Dvorak, George J., Jian Zhang, and Olcay Canyurt. "Adhesive Joints for Composite Sandwich Structures." In ASME 2000 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2000. http://dx.doi.org/10.1115/imece2000-2034.

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Abstract A new approach is explored for joining of thick, woven E-glass/vinyl ester composite laminated plates to steel or composite plates, with applications in naval ship structures. Adhesive is applied along through-the-thickness contoured interfaces, employing tongue-and-groove geometry. Both experimental and finite element modeling results are presented. They show that adhesively bonded tongue-and-groove joints between steel and composite plates loaded in monotonically increasing longitudinal tension, are stronger than conventional strap joints even in relatively thin plates. In particula

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Diveyev, Bohdan M., Ihor B. Butyter, and Natalie N. Shcherbyna. "High Order Theories for Elastic Modules Identification of Composite Plates." In ASME 2008 9th Biennial Conference on Engineering Systems Design and Analysis. ASMEDC, 2008. http://dx.doi.org/10.1115/esda2008-59278.

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The study aims to predict elastic and damping properties of composite laminated plates from the measured dynamical properties. Elastic constants of laminates and damping properties have been determined by using an identification procedure based on experiment design, and multi-level theoretical approach. The present paper is the first attempt at proposing a novel adaptive procedure to derive stiffness parameters from forced sandwich plate’s vibration experiments.

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Katariya, Pankaj, and Subrata Kumar Panda. "Simulation Study of Transient Responses of Laminated Composite Sandwich Plate." In ASME 2017 Gas Turbine India Conference. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/gtindia2017-4846.

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In this article, the transient responses of the laminated composite sandwich plate structure are obtained numerically using the commercial finite element package to reduce the computational cost without hampering the accuracy. The plate structure is discretized using the available shell element (SHELL281) from ANSYS library. In order to compute the responses, an ANSYS parametric design language code has been developed based on the finite element steps and Newmark integration technique. The model accuracy and stability have been checked and few numerical examples have been solved. Finally, the

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Araújo, A. L., C. M. Mota Soares, C. A. Mota Soares, et al. "Parameter Estimation in Hybrid Active-Passive Laminated Sandwich Composite Structures." In PROCEEDINGS OF THE 2ND INTERNATIONAL SYMPOSIUM ON COMPUTATIONAL MECHANICS AND THE 12TH INTERNATIONAL CONFERENCE ON THE ENHANCEMENT AND PROMOTION OF COMPUTATIONAL METHODS IN ENGINEERING AND SCIENCE. AIP, 2010. http://dx.doi.org/10.1063/1.3452037.

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Vaidya, Uday K., Anthony N. Palazatto, and L. N. B. Gummadi. "Low Velocity Impact Response and Nondestructive Evaluation of Sandwich Composite Structures." In ASME 1997 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 1997. http://dx.doi.org/10.1115/imece1997-1045.

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Abstract Composite sandwich constructions offer light weight and high bending stiffness advantages for aerospace and automotive applications among other structures. The use of a hollow truss core or z-fiber pin core is a new concept in sandwich composites, where the core is hollow and accessible, thereby providing space advantages for fuel cells and/or electronic assemblies besides from possessing high shear and axial stiffness. The z-fiber pins are oriented at predetermined geometry’s and penetrate into the laminated facesheets making-up the sandwich composite. In the reference (Palazatto et.

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Wang, C. M., K. K. Ang, and C. Wang. "Vibration of Skew Sandwich Plates With Laminated Facings." In ASME 1997 Turbo Asia Conference. American Society of Mechanical Engineers, 1997. http://dx.doi.org/10.1115/97-aa-050.

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A Rayleigh-Ritz analysis is presented for the free vibration of skew sandwich plates composed of an orthotropic core and laminated facings. By proposing a set of Ritz functions consisting of the product of mathematically complete polynomial functions and the the boundary equations raised to appropriate powers, the Rayleigh-Ritz method can be automated to handle such composite plates with any combination of edge conditions. For convenience and better accurarcy, the Ritz formulation was derived in the skew coordinate system. Vibration frequencies of rectangular plates (a special case of skew pla

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Birman, Victor, and Larry W. Byrd. "On the Prediction of Damping in Composite and Sandwich Structures." In ASME 2001 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2001. http://dx.doi.org/10.1115/imece2001/amd-25409.

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Abstract The paper outlines two methodologies for the analytical evaluation of the loss factor in composite laminates and in sandwich structures. One of these methods is based on the analysis of free vibrations, while the second approach utilizes mechanics of materials. The loss factor can be predicted both for specially orthotropic as well as for generally orthotropic laminae, subjected to axial stresses and/or transverse shear. The results for the loss factor of the laminae are in good agreement with available experimental data. As follows from numerical examples, the loss factor of polymer-

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Albernaz, Jessica. "Bending Analysis of Laminated Composite Sandwich Plates Reinforced with Carbon Nanotube Forests." In 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/6.2009-200.

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Reports on the topic "Laminated and sandwich composite"

1

Perez-Rivera, Anthony, Jonathan Trovillion, Peter Stynoski, and Jeffrey Ryan. Simulated barge impacts on fiber-reinforced polymers (FRP) composite sandwich panels : dynamic finite element analysis (FEA) to develop force time histories to be used on experimental testing. Engineer Research and Development Center (U.S.), 2024. http://dx.doi.org/10.21079/11681/48080.

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The purpose of this study is to evaluate the dynamic response of fiber-reinforced polymer (FRP) composite sandwich panels subjected to typical barge impact masses and velocities to develop force time histories that can be used in controlled experimental testing. Dynamic analyses were performed on FRP composite sandwich panels using the finite element method software Abaqus/Explicit. The “traction-separation” law in the Abaqus software is used to define the cohesive surface interaction properties to evaluate the damage between FRP composite laminate layers as well as the core separation within

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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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Spera, D. A., J. B. Esgar, M. Gougeon, and M. D. Zuteck. Structural properties of laminated Douglas fir/epoxy composite material. Office of Scientific and Technical Information (OSTI), 1990. http://dx.doi.org/10.2172/6492500.

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Barton, Oscar, Ratcliffe Jr., and Colin P. Fundamental Frequency of a Composite Sandwich Plate Containing Woven Layers. Defense Technical Information Center, 1997. http://dx.doi.org/10.21236/ada359126.

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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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Blake, H. W., and J. M. Starbuck. Hydrostatic testing of thick laminated composite cylinders for performance model validation. Office of Scientific and Technical Information (OSTI), 1993. http://dx.doi.org/10.2172/10151163.

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Hammerand, Daniel Carl. Critical time step for a bilinear laminated composite Mindlin shell element. Office of Scientific and Technical Information (OSTI), 2004. http://dx.doi.org/10.2172/919205.

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Sandhu, R. S., W. E. Wolfe, R. L. Sierakowski, C. C. Chang, and H. R. Chu. Finite Element Analysis of Free-Edge Delamination in Laminated Composite Specimens. Defense Technical Information Center, 1991. http://dx.doi.org/10.21236/ada251659.

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Blake, H. W., and J. M. Starbuck. Hydrostatic testing of thick laminated composite cylinders for performance model validation. Office of Scientific and Technical Information (OSTI), 1993. http://dx.doi.org/10.2172/6855310.

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Stephens, Max. Numerical and Experimental Analysis of Composite Sandwich Links for the LCF System. Portland State University Library, 2000. http://dx.doi.org/10.15760/etd.579.

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