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Journal articles on the topic 'Laminated materials Composite materials'

Author: Grafiati

Published: 4 June 2021

Last updated: 13 February 2022

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1

Vieira Carneiro, C. A., and M. A. Savi. "Modelling and simulation of the delamination in composite materials." Journal of Strain Analysis for Engineering Design 35, no. 6 (2000): 479–92. http://dx.doi.org/10.1243/0309324001514242.

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Delamination is a phenomenon characterized by the loss of adhesion between two adjacent laminae. This is a damage process frequently observed in composite materials and it may cause either loss of structural stiffness or total failure of the laminate. This contribution presents a model to describe composite delamination. The proposed model considers a laminate with a finite thickness interlayer. Interlaminar stresses are evaluated from a modified lamination theory. This result is used as input in the constitutive adhesion model which describes the damage evolution of the interlayer. An iterati

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Abrate, Serge. "Impact on Laminated Composite Materials." Applied Mechanics Reviews 44, no. 4 (1991): 155–90. http://dx.doi.org/10.1115/1.3119500.

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Laminated composite materials are used extensively in aerospace and other applications. With their high specific modulus, high specific strength, and the capability of being tailored for a specific application, these materials offer definite advantages compared to more traditional materials. However, their behavior under impact is a concern, since impacts do occur during manufacture, normal operations, or maintenance. The situation is critical for impacts which induce significant internal damage, undetectable by visual inspection, that cause large drops in the strength and stability of the str

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Aveiga, David, and Marcelo L. Ribeiro. "A Delamination Propagation Model for Fiber Reinforced Laminated Composite Materials." Mathematical Problems in Engineering 2018 (June 19, 2018): 1–9. http://dx.doi.org/10.1155/2018/1861268.

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The employment of composite materials in the aerospace industry has been gradually considered due to the fundamental lightweight and strength characteristics that this type of materials has. The science material and technological progress reached matched perfectly with the requirements for high-performance materials in aircraft and aerospace structures; thus, the development of primary structure elements applying composite materials became something very convenient. It is extremely important to pay attention to the failure modes that influence composite materials performances, since these fail

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ALLEN, D. ALBERT, G. RAMANAN, R. R. NEELA RAJAN, and A. K. DARWINS. "Experimental Study on Change in Mechanical Characteristics of E-Glass Fibre Reinforced Epoxy Composite by Adding Carbon Nanotube Layers." Asian Journal of Chemistry 31, no. 6 (2019): 1251–54. http://dx.doi.org/10.14233/ajchem.2019.21874.

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Polymer composite reinforced with fiber materials have always proven its superior significant enactment over numerous traditional materials, considering their incomparable strength to weight ratio and stiffness. Carbon nanotubes usage in glass-fiber reinforced polymer has high potential in changing the characteristics of composite laminates. Carbon nanotubes have engrossed composite fraternity in exploring the opportunity of utilizing them as a supplementary reinforcement in fiber reinforced polymer composites. This study examines the mechanical characters of glass-fiber reinforced polymer wit

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Ramadhan, Redha Akbar, Muhamad Giri Suada, and Hendri Syamsudin. "A FINITE ELEMENT ANALYSIS OF CRITICAL BUCKLING LOAD OF COMPOSITE PLATE AFTER LOW VELOCITY IMPACT." Jurnal Teknologi Dirgantara 18, no. 2 (2020): 195. http://dx.doi.org/10.30536/j.jtd.2020.v18.a3328.

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Composite is a material formed from two or more materials that macroscopically alloyed into one material. Nowadays, composite has been generally applied as lightweight structure of aircraft. This is due to the fact that composites having high strength-to-weight ratio. It means the composites have the capability to take on various loads, despite their lightweight property.Laminate composite is one type of composite that has been generally used in aircraft industries. This type of composite is susceptible to low-velocity impact induced damage. This type of damage can be happening in manufacture,

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Xu, Jian, Pei Xian Zhu, Hui Yu Ma, and Sheng Gang Zhou. "Characterisation of Ti-Al and Ti-Cu Laminated Composite Electrode Materials." Advanced Materials Research 194-196 (February 2011): 1667–71. http://dx.doi.org/10.4028/www.scientific.net/amr.194-196.1667.

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We proposed using Ti-Al and Ti-Cu laminated composites instead of single Ti electrode metals, as well as studied the difference in performance between laminated composite electrode materials and pure-Ti electrode. The analysis of the conductivity and electrochemical performance of electrode matrix material indicates the result that the improvement of matrix material by using Ti-Al and Ti-Cu laminated composites, better performance for conductivity of electrode, and be beneficial to homogenize the electrode surface potential and current distribution and promote electrocatalytic activity between

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Hajikhani, Milad, Amir Refahi Oskouei, Mehdi Ahmadi Najaf Abadi, Amir Sharifi, and Mohammad Heidari. "Progressive Fracture Evaluation in Composite Materials by Acoustic Emission Technique." Key Engineering Materials 465 (January 2011): 535–38. http://dx.doi.org/10.4028/www.scientific.net/kem.465.535.

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Glass/polyester and glass/epoxy laminated composites widely used in structures and have very near properties. These composite laminates have poor inter-laminar fracture resistance and suffer extensive damage by delamination cracking when subjected to out of plane loading and hence are vulnerable to delamination. The presence of delamination in the composite material may reduce the overall stiffness. Structural design and nondestructive test techniques have evolved as increased emphasis has been placed on the durability and damage tolerance of these materials. There are several methods used to

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Taheri-Behrooz, Fathollah, and Nima Bakhshi. "Neuber’s rule accounting for the material nonlinearity influence on the stress concentration of the laminated composites." Journal of Reinforced Plastics and Composites 36, no. 3 (2016): 214–25. http://dx.doi.org/10.1177/0731684416680302.

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Since holes comprise the necessary features of many structural components, a comprehensive understanding of the behavior of composite plates containing an open hole is a crucial step in their design process. In the present manuscript, an extensive numerical study has been conducted in order to investigate the effects of material nonlinearity on the stress distribution and stress concentration factors in unidirectional and laminated composite materials. To attain this objective, various models with different configurations were studied. In unidirectional composites, the maximum deviation of str

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Luo, Shen-Yi, and Faruk Taban. "Deformation of Laminated Elastomer Composites." Rubber Chemistry and Technology 72, no. 1 (1999): 212–24. http://dx.doi.org/10.5254/1.3538791.

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Abstract Flexible elastomer composites subjected to finite deformation are usually associated with significant fiber re-orientation and configuration change which cannot be described by classical composite lamination theory. Utilizing the Lagrangian description and a strain-energy density approach, this work presents a set of 2-D constitutive equations in terms of the overall deformation of laminated composites. This model includes both geometric and material nonlinearities of the laminate. Interlaminar shear deformation is addressed but not studied in this analysis. Theoretical predictions ha

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Boria, Simonetta, and Alessandro Scattina. "Energy absorption capability of laminated plates made of fully thermoplastic composite." Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science 232, no. 8 (2018): 1389–401. http://dx.doi.org/10.1177/0954406218760059.

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The behaviour of composites materials, made of synthetic fibres embedded in a thermoplastic resin, subjected to low velocity impacts, was largely studied in the past. However, in the last years, the use of thermoplastic composites has been increased due to the considerable advantages in terms of recyclability of this family of materials. Thermoplastic composites are composed of polymers with different material’s structure if compared to the more traditional thermoset composite. Consequently, the behaviour of these materials can be different in some loading conditions. Moreover, considering the

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Chen, Z., J. J. Mecholsky, and S. Hu. "Effect of interface design on high-temperature failure of laminated composites." Journal of Materials Research 11, no. 8 (1996): 2035–41. http://dx.doi.org/10.1557/jmr.1996.0256.

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The fracture strength and toughness of alumina can be increased by lamination with strategically placed nickel layers and with a modified Ni/Al2O3 interface through tape casting. In order to examine the potential of this type of laminated composite in high temperature applications, the laminates were tested at elevated temperatures. This paper describes how a modified tortuous interface, instead of a smooth interface, increases the creep resistance of the laminates. Interface modification can control high temperature laminate behavior and is critical to successful composite design.

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bin Yaakob, Mohd Yuhazri, T. T. T. Jennise, H. Sihombing, N. Mohamad, S. H. Yahaya, and M. Y. A. Zalkis. "Water Absorption and Thickness Swelling of Laminated Composite after Cured at Different Angle." Applied Mechanics and Materials 465-466 (December 2013): 86–90. http://dx.doi.org/10.4028/www.scientific.net/amm.465-466.86.

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Moisture absorption is a very important factor in polymers and composite materials used for hull manufacture and stability in marine environment. High water absorption of the material will affects the mechanical properties and stability in composite. This research is carried out to study the feasibility of the gravity effects on curing position of the laminated composite structures to enhance the curing space needed. Vertical cured laminate having almost similar properties with common horizontal cured laminate able to save much space in composite industry. Horizontal cured laminates filled up

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Ali, Mubarak, S. C. Joshi, and Mohamed Thariq Hameed Sultan. "Palliatives for Low Velocity Impact Damage in Composite Laminates." Advances in Materials Science and Engineering 2017 (2017): 1–16. http://dx.doi.org/10.1155/2017/8761479.

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Fibre reinforced polymer laminated composites are susceptible to impact damage during manufacture, normal operation, maintenance, and/or other stages of their life cycle. Initiation and growth of such damage lead to dramatic loss in the structural integrity and strength of laminates. This damage is generally difficult to detect and repair. This makes it important to find a preventive solution. There has been abundance of research dealing with the impact damage evolution of composite laminates and methods to mitigate and alleviate the damage initiation and growth. This article presents a compre

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Jennise, T. T. T., Mohd Yuhazri bin Yaakob, H. Sihombing, N. Mohamad, S. H. Yahaya, and M. Y. A. Zalkis. "Hardness of Laminated Composite for Different Angle Cured Positions under Influence of Gravity Effects." Applied Mechanics and Materials 446-447 (November 2013): 1566–69. http://dx.doi.org/10.4028/www.scientific.net/amm.446-447.1566.

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Utilization of high tech engineering materials such as composites has been extensively applied in the industries of civil, mechanical and aerospace due to their favourable characteristic such as high stiffness to weight ratio, improve corrosion and environmental resistance and potential reduction of processing. This research is carried out to study the feasibility of laminated composite after cured at different angle due to gravity effects to enhance the curing space required. Vertically cured laminate having similar or improved properties with common horizontally cured laminate to save much s

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Hou, J. P., and C. Ruiz. "Soft body impact on laminated composite materials." Composites Part A: Applied Science and Manufacturing 38, no. 2 (2007): 505–15. http://dx.doi.org/10.1016/j.compositesa.2006.02.018.

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Muric-Nesic, Jelena, Z. Stachurski, Paul Compston, and N. Noble. "Effect of Vibrations on Void Content in Composite Materials." Advanced Materials Research 32 (February 2008): 145–48. http://dx.doi.org/10.4028/www.scientific.net/amr.32.145.

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Eliminating common defects such as voids, bubbles and poor adhesion at interfaces will increase the quality of laminated sandwich composite structure. We are experimenting and analyzing the effect of mechanical vibrations applied to the curing system of composite materials production, particularly on minimizing void content. The range of frequency of vibrations covered was from 2Hz to 8kHz, for different period of vibrations. The composite laminates were made by hand lay-up using glass fibres and vinyl-ester resin, and examined under a microscope to determine types and quantity of defects. The

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Luccioni, Bibiana M. "Constitutive Model for Fiber-Reinforced Composite Laminates." Journal of Applied Mechanics 73, no. 6 (2006): 901–10. http://dx.doi.org/10.1115/1.2200654.

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Nowadays, conventional materials have been progressively replaced by composite materials in a wide variety of applications. Particularly, fiber reinforced composite laminates are widely used. The appropriate design of elements made of this type of material requires the use of constitutive models capable of estimating their stiffness and strength. A general constitutive model for fiber reinforced laminated composites is presented in this paper. The model is obtained as a generalization of classical mixture theory taking into account the relations among the strains and stresses in the components

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Dolgikh, D. A., and M. A. Tashkinov. "Investigation of damage accumulation and delamination propagation in polymer composite materials based on two-level fracture models." PNRPU Mechanics Bulletin, no. 4 (December 15, 2020): 74–85. http://dx.doi.org/10.15593/perm.mech/2020.4.07.

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The work is devoted to the study of deformation and fracture processes occurring in layered composites under combined loading modes. The aim of the work is numerical analysis of different modes of fracture, which are simultaneously realized in the samples of laminated composite material. Models of laminated composite material with imitation of technological defects in the form of material debonding are constructed. The delamination process is implemented using the virtual crack closure technique. The processes of damage accumulation and fracture of laminated composites are set on the basis of

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Carreño, Fernando, M. Pozuelo, José A. Jiménez, and Oscar A. Ruano. "Bend and Shear Tests: Suitable Methods for Mechanical Characterization of Laminated Composite Materials." Materials Science Forum 539-543 (March 2007): 901–6. http://dx.doi.org/10.4028/www.scientific.net/msf.539-543.901.

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Bend and shear tests were used to characterize the improvement in impact behavior of various ultrahigh carbon steel laminated composites. These tests turned out to deliver much more useful information about the mechanical properties of the laminates than the Charpy impact tests and were especially interesting for characterization of laminates of very high toughness values. The toughness of the various laminates was controlled by the rolling conditions that determined the quality of the bond and the appearance of delamination by the interfaces. The bend test allows determination of yield and ma

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Abrate, Serge. "Impact on Laminated Composites: Recent Advances." Applied Mechanics Reviews 47, no. 11 (1994): 517–44. http://dx.doi.org/10.1115/1.3111065.

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Impact damage in structures made out of composite materials is a major concern since such damage can be introduced during the life of the structure, and its mechanical properties can be drastically reduced as a result. In a previous review of the literature on impact on composite materials, this author considered 285 published before 1989. In this article over 300 articles most of which appeared after 1989 are reviewed. These figures indicate that this is a very active area of research, and the present paper seeks to present a comprehensive view of the latest developments. Taken together, thes

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Glukhov, A. Yu. "Axisymmetric waves in laminated composite incompressible materials with initial stresses under the slipping of layers." Reports of the National Academy of Sciences of Ukraine, no. 10 (November 16, 2016): 42–46. http://dx.doi.org/10.15407/dopovidi2016.10.042.

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Yoon, Sung Won, and Chang Wook Park. "Laminated design for the application of composite materials for ship radar mast." International Journal of Modern Physics B 35, no. 14n16 (2021): 2140039. http://dx.doi.org/10.1142/s0217979221400397.

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The purpose of this study is to determine the correct estimation of laminated design for composite materials applied to a ship radar mast. Recently, as the IMO’s environmental regulations have been strengthened to increase the energy efficiency of ships, the IMO has also begun to consider operational economics such as energy reduction through lightening the hull. Demand for lighter weight technology using composite materials is increasing. Examples would include lightweight large structures using composite materials, composite materials replacing metal design parts, and polymer composite mater

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Christoforo, André L., Maria F. do Nascimento, Tulio H. Panzera, Sérgio L. M. Ribeiro Filho, and Francisco A. R. Lahr. "Homogeneous Pinus sp. particle boards reinforced with laminated composite materials." Engenharia Agrícola 36, no. 3 (2016): 558–65. http://dx.doi.org/10.1590/1809-4430-eng.agric.v36n3p558-565/2016.

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ABSTRACT This study aimed to evaluate the mechanical performance of laminated composite materials (fiberglass, carbon, sisal, palm fiber) in epoxy matrix as reinforcement in wood particleboards of Pinus sp. with bicomponent polyurethane resin from castor oil. Modulus of elasticity (MOE) and modulus of rupture (MOR) were investigated using a three-point bending test. Single-layered laminated plates were used to reinforce traction of specimens obtained from boards. MOE and MOR of materials developed without reinforcements exceeded limits in ABNT standards both NBR 12810-2:2002 and A208.1:199, pr

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Pelaez, Jose Ignacio, Jose Antonio Gomez-Ruiz, Jorge Veintimilla, Gustavo Vaccaro, and Patricia Witt. "Memetic Computing Applied to the Design of Composite Materials and Structures." Mathematical Problems in Engineering 2017 (2017): 1–16. http://dx.doi.org/10.1155/2017/4723863.

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Presently, there exists an important need for lighter and more resistant structures, with reduced manufacturing costs. Laminated polymers are materials which respond to these new demands. Main difficulties of the design process of a composite laminate include the necessity to design both the geometry of the element and the material configuration itself and, therefore, the possibilities of creating composite materials are almost unlimited. Many techniques, ranging from linear programming or finite elements to computational intelligence, have been used to solve this type of problems. The aim of

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Babanli, Mustafa, and Yusif Tanriverdiyev. "RESEARCH OF Al AND Mg MATRİX HYBRİD LAMİNATED COMPOSİTE MATERİALS." ETM - Equipment, Technologies, Materials 05, no. 01 (2021): 11–15. http://dx.doi.org/10.36962/etm0501202011.

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The main purpose of this research is to select suitable matrices and fillers for the preparation of composites that meet modern requirements to meet the needs of a rapidly growing industry. Studies in various databases have shown that metal-matrix hybrid laminated composite materials, mainly aluminum and magnesium alloy plates, are used as matrix materials, while carbon-based nanomaterials are used as fillers. Keywords: composition, matrix, aluminum, magnesium.

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Shokrieh, Mahmood M., and Saeed Akbari R. "Simulation of slitting method for calculation of compliance functions of laminated composites." Journal of Composite Materials 46, no. 9 (2011): 1101–9. http://dx.doi.org/10.1177/0021998311415725.

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In this research, the process of slitting with an assumed residual stress distribution is simulated to calculate compliance functions of laminated composites. The primary aim of this article is to investigate different parameters influencing the calculation of compliance coefficients for laminated composites using a finite element model. First, using two- and three-dimensional finite element models, the process of slitting in isotropic materials for calculating the compliance coefficients is simulated. The results show a complete agreement between the two models. Also, the results of simulatio

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Ali, Hafiz Tauqeer, Roya Akrami, Sakineh Fotouhi, Farzad Pashmforoush, Cristiano Fragassa, and Mohammad Fotouhi. "EFFECT OF THE STACKING SEQUENCE ON THE IMPACT RESPONSE OF CARBON-GLASS/EPOXY HYBRID COMPOSITES." Facta Universitatis, Series: Mechanical Engineering 18, no. 1 (2020): 069. http://dx.doi.org/10.22190/fume191119010a.

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This paper investigates low-velocity impact response of Quasi Isotropic (QI) hybrid carbon/glass fiber reinforced polymer composites with alternate stacking sequences. Cross-ply woven carbon and glass fibers were used as reinforcing materials to fabricate sandwiched and interlayer hybrid composites. For comparison, the laminates containing only-carbon and only-glass fibers were also studied. Drop weight test was used to impact the samples. The images captured by a normal camera demonstrated that localized damages (delamination) existed within plies. The hybrid laminates had smaller load drops,

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Beyeler, E. P., and S. I. Gu¨c¸eri. "Thermal Analysis of Laser-Assisted Thermoplastic-Matrix Composite Tape Consolidation." Journal of Heat Transfer 110, no. 2 (1988): 424–30. http://dx.doi.org/10.1115/1.3250502.

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A novel approach to producing composite parts using thermoplastic-matrix tapes is described. A thermal analysis is presented for the case of focused heat sources such as lasers for melting and consolidating the prepregs in a continuous manufacturing process. A numerical grid generation method is employed to account for the complex geometry of the solution domain. Heat transfer is modeled using an orthotropic domain made of two-dimensional, continuous fiber anisotropic laminates. Heat of crystallization melting/solidification are included in the form of a heat generation term. The temperature d

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Zhang, Wei, Wen Yong Tang, Ying Chao Pu, and Sheng Kun Zhang. "Ultimate Strength Analysis of Ship Hulls of Continuous Basalt Fiber Composite Materials." Advanced Materials Research 150-151 (October 2010): 736–40. http://dx.doi.org/10.4028/www.scientific.net/amr.150-151.736.

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Based on effective composite material failure criteria and property limited degradation model, axial compressive ultimate strength of composite laminated stiffened panels are analyzed by nonlinear laminated degenerated 3D finite element analysis, which is based on incremental continuum-based updated Lagrangian formulation. Comparison between analytical solutions and test results in this article indicates that this article provides an effective and practical method to evaluate the axial compressive ultimate strength of composite laminated stiffened panels. Using this method, ultimate strength o

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Abouhamzeh, Sinke, and Benedictus. "Prediction Models for Distortions and Residual Stresses in Thermoset Polymer Laminates: An Overview." Journal of Manufacturing and Materials Processing 3, no. 4 (2019): 87. http://dx.doi.org/10.3390/jmmp3040087.

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This paper reviews predictive models developed for the development of residual stresses and shape distortions during the manufacturing of thermoset polymeric/composite materials. Different sources that produce residual stresses and shape changes in the laminated panels are described and reviewed. An overview is presented on the characterisation and predictions of the phenomena resulting in residual stresses. The focus will be on the models accounting for the parameters during the cure cycle of the thermoset composite materials published in the literature from 2005 until 2018. The material type

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Sol, Hugo, Hubert Rahier, and Jun Gu. "Prediction and Measurement of the Damping Ratios of Laminated Polymer Composite Plates." Materials 13, no. 15 (2020): 3370. http://dx.doi.org/10.3390/ma13153370.

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Laminated composites materials are mostly used in dynamically loaded structures. The design of these structures with finite element packages is focused on vibrations, elastic deformations and failure control. Damping is often neglected because of its assumed secondary importance and also because of dearth of information on relevant material properties. This trend is prone to change as it is now realised that damping plays an increasingly important role in vibration comfort, noise radiation and crash simulations. This paper shows in a first step how to identify the orthotropic elastic and dampi

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Wang, H., and T. Vu-Khanh. "Low-Velocity Impact Damage in Laminated Composite Materials." Key Engineering Materials 141-143 (September 1997): 277–304. http://dx.doi.org/10.4028/www.scientific.net/kem.141-143.277.

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O., BADIE, and SALLAM T. "BONDING AND PROCESSING TECHNIQUE OF LAMINATED COMPOSITE MATERIALS." International Conference on Aerospace Sciences and Aviation Technology 10, ASAT CONFERENCE (2003): 1–17. http://dx.doi.org/10.21608/asat.2013.24455.

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Matsumoto, Kin'ya, Masaru Zako, Atsushi Yokoyama, and Tetsuya Tsujikami. "Transient Heat Conduction Analysis for Laminated Composite Materials." Transactions of the Japan Society of Mechanical Engineers Series A 60, no. 573 (1994): 1250–54. http://dx.doi.org/10.1299/kikaia.60.1250.

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Narita, Yoshihiro. "Advancement of Structural Optimization in Laminated Composite Materials." Proceedings of OPTIS 2016.12 (2016): SP1. http://dx.doi.org/10.1299/jsmeoptis.2016.12.sp1.

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Golubev, A. I. "Calculation of the composition of laminated composite materials." Fibre Chemistry 27, no. 4 (1996): 264–65. http://dx.doi.org/10.1007/bf00572804.

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Khoroshun, L. P., and E. N. Shikula. "Nonlinear deformation of laminated composite materials with microfailures." International Applied Mechanics 32, no. 9 (1996): 697–701. http://dx.doi.org/10.1007/bf02083634.

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Nawab, Yasir, Frédéric Jaquemin, Pascal Casari, Nicolas Boyard, and Vincent Sobotka. "Evolution of chemical and thermal curvatures in thermoset-laminated composite plates during the fabrication process." Journal of Composite Materials 47, no. 3 (2012): 327–39. http://dx.doi.org/10.1177/0021998312440130.

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Residual deformations and stresses formation in the thermoset-laminated composite is a frequently studied subject in the recent years. During fabrication, the laminated composites undergo chemical deformation during cross-linking and thermal deformation while cooling. In thin laminates, due to large displacements and complex evolution of shape, these deformations can only be explained by using nonlinear strain–displacement relationship. In the present article, we calculated together for the first time, the thermal and chemical deformations occurring in carbon/epoxy laminates by considering a n

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Marzuki, Haslan Fadli Ahmad, Engku Ahmadhilmi Engku Ubaidillah, Sivakumar A/l Sivarasa, Mohd Syamsul, and Mariatti Jaafar. "Study on Effect of Fiber Orientation on Flexural Properties of Glass Fiber Reinforced Epoxy Composite Laminates for Structural Applications." Solid State Phenomena 301 (March 2020): 227–37. http://dx.doi.org/10.4028/www.scientific.net/ssp.301.227.

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Composite laminate design is an important procedure in defining the mechanical properties of laminated composite structure to be used in multi-directional service loading application. Composite technologies or manufacturers who is lack of knowledge regarding the importance of laminate design, tend to develop a composite structure that will collapse or fail below the service requirement. The purpose of this study is to determine the effect of fiber orientation on flexural properties of the designed glass fiber reinforced epoxy laminated composite. Six sets of laminates with different fiber orie

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Han, Zhaohui, Peixian Zhu, Yuzhong Guo, and Shenggang Zhou. "Study on the Interface and Performance of Ti-Al Laminated Composite Electrode Materials." Journal of New Materials for Electrochemical Systems 18, no. 3 (2015): 159–64. http://dx.doi.org/10.14447/jnmes.v18i3.363.

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The Ti-Al laminated composite materials had been prepared by hot press diffusion bonding in this article, then, treated for different thickness of Al layer in the same process conditions. The change of composite material structure is influences on the performance of Ti-Al were investigated by SEM, HRTEM, electrochemical workstation and so on. The results show that it has the characteristics of the composite's interface and the completion of "metallurgy like" integration between Ti and Al, the chang of matrix structure design of traditional Ti electrode is good for enhance the electrochemical p

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Kazemi, M., and G. Verchery. "A Methodology for Optimal Design of Composite Laminates Using Polar Formalism." Journal of Mechanics 32, no. 3 (2016): 255–66. http://dx.doi.org/10.1017/jmech.2015.98.

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AbstractAn innovative optimization technique is presented for the design of composite laminated plates subjected to in-plane loads. A list of quasi-homogeneous laminates that can be used as angle-ply materials is proposed as a comprehensive solution for optimum lay-up. Two optimization procedures are performed: Dimensioning of the flexural stiffness and the elastic modulus, which provides the optimal orientations for the layers and offer highest in-plane resistance to composite laminated structures. The polar formalism for plane anisotropy is used to represent the flexural stiffness and elasti

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Al-Madani, Ramadan A., M. Jarnaz, K. Alkharmaji, and M. Essuri. "Finite Element Modeling of Composites System in Aerospace Application." Applied Mechanics and Materials 245 (December 2012): 316–22. http://dx.doi.org/10.4028/www.scientific.net/amm.245.316.

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The characteristics of composite materials are of high importance to engineering applications; therefore the increasing use as a substitute for conventional materials, especially in the field of aircraft and space industries. It is a known fact that researchers use finite element programs for the design and analysis of composite structures, use of symmetrical conditions especially in complicated structures, in the modeling and analysis phase of the design, to reduce processing time, memory size required, and simplifying complicated calculations, as well as considering the response of composite

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Pazhanivel, K., G. B. Bhaskar, S. Arunachalam, V. Hariharan, and A. Elayaperumal. "Low Velocity Impact Analysis on GFRP Laminates under Different Temperatures." Applied Mechanics and Materials 110-116 (October 2011): 632–36. http://dx.doi.org/10.4028/www.scientific.net/amm.110-116.632.

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Composite materials have a number of properties that make them attractive for use in aerospace applications. The impact behavior of fiber reinforced composite materials is much more complex than conventional metallic structures due to a number of different failure modes on the inter laminar and intra laminar level. The aim of this study is to investigate the effects of temperature and thermal residual stresses on the impact behavior and damage of glass/epoxy laminated composites. To this end, thermal stress analyses of the laminates with lay-ups [90/0/0/90] s, [90/0/45/45] s, [0/90/45/-45] s,

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Márquez Costa, Juan Pablo, Vincent Legrand, and Sylvain Fréour. "Durability of Composite Materials under Severe Temperature Conditions: Influence of Moisture Content and Prediction of Thermo-Mechanical Properties During a Fire." Journal of Composites Science 3, no. 2 (2019): 55. http://dx.doi.org/10.3390/jcs3020055.

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The main objective of the present study was to develop a fire thermal model able to predict the evolution of the temperature and decomposition gradient across a laminated composite structure when exposed to fire. The thermal response of composite laminate made of organic polymer matrix was investigated under severe temperature conditions as samples were exposed to high temperatures up to 750 °C. The highlight is that a behavior law for water is included in our thermo-mechanical model to estimate effects due to a moisture content field on the thermal response of composite laminates. In particul

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Evran, Savaş. "Numerical and statistical buckling analysis of laminated composite plates with functionally graded fiber orientation angles." Polymers and Polymer Composites 28, no. 7 (2020): 502–12. http://dx.doi.org/10.1177/0967391120936029.

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The aim of this numerical and statistical study was to investigate the buckling analysis of laminated composite plates containing functionally graded fiber orientation angles. The laminated composite plates had functionally graded fiber orientation angles based on Taguchi’s L18 (21 × 32) orthogonal array. The fiber orientation angles were considered to be control factors. Numerical analyses were performed using finite element software ANSYS. The optimum critical buckling load and the effects of fiber orientation angles for maximum data were determined using the analysis of the signal-to-noise

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Hwang, Do Yeon, Akira Shimamoto, and Kazuyoshi Takayama. "High-Velocity Impact Characteristic of Carbon Fiber Reinforced Plastic Laminates Using Ballistic Range." Key Engineering Materials 324-325 (November 2006): 1071–74. http://dx.doi.org/10.4028/www.scientific.net/kem.324-325.1071.

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Recently, high-performance hybrid composites have been used for various applications which require the high strength, high stiffness and low weight. There are growing needs in an automotive, an aircraft, and military applications for composite materials since they have good structural characteristics. They also have good penetration resistance and structural integrity after impact. In order to clarify the mechanism of high-speed destruction for composite materials, this study examined the penetration resistance and the fracture behavior of CFRP (Carbon Fiber Reinforced Plastic) Laminates by us

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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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Dudek, P., and A. Rapacz-Kmita. "Rapid Prototyping: Technologies, Materials and Advances." Archives of Metallurgy and Materials 61, no. 2 (2016): 891–96. http://dx.doi.org/10.1515/amm-2016-0151.

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AbstractIn the context of product development, the term rapid prototyping (RP) is widely used to describe technologies which create physical prototypes directly from digital data. Recently, this technology has become one of the fastest-growing methods of manufacturing parts. The paper provides brief notes on the creation of composites using RP methods, such as stereolithography, selective laser sintering or melting, laminated object modelling, fused deposition modelling or three-dimensional printing. The emphasis of this work is on the methodology of composite fabrication and the variety of ma

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You, Feng Xiang, Fei Zhang, and Buo Lei Zuo. "Spline-Based Finite Element Analysis in Composite Laminates Mechanical Properties." Applied Mechanics and Materials 138-139 (November 2011): 673–80. http://dx.doi.org/10.4028/www.scientific.net/amm.138-139.673.

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The geometric parameters of the composite laminate in the engineering structure tend to have random properties. It is of great significance on how to study sensitivity of random parameters of laminated plates and carry on the optimized analysis to the parameteranalys when accurately estimating the reliability of structural design. According to the first order shear deformation theory, by using the spline finite element method, we can infer and the establish a laminated plate vibration equation, the stiffness matrix, mass matrix, proportional damping matrix, before making solution of the antisy

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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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