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Relevant bibliographies by topics / Composite deformation

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Academic literature on the topic 'Composite deformation'

Author: Grafiati

Published: 4 June 2021

Last updated: 8 February 2022

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Journal articles on the topic "Composite deformation"

1

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 (February 22, 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 nonlinear geometrical approach to understand the evolution of shape and hence residual stresses induced during fabrication process. The effect of fibre fraction on the chemical and thermal deformations is studied as well.

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Garbacz, G., and L. Kyzioł. "Application of metric entropy for results interpretation of composite materials mechanical tests." Advances in Materials Science 17, no. 1 (March 1, 2017): 70–81. http://dx.doi.org/10.1515/adms-2017-0006.

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Abstract In this paper the results of mechanical studies of the Aropol 536 composite on the epoxy-resin base are described. The aim of the studies was to measure elastic-plastic changes in the composite during its deformation. The obtained results were analyzed using Kolmogorov-Sinai metric entropy. The entropy was computed applying phase portraits reconstructed from a phase plane using delayed coordinates. Resolution of the particular experimental setup limits the number of the acquired data points, i.e., from several to tens of thousands of points and it has significant influence on accuracy of the obtained results. In conclusion, in the tested composites elastic-plastic deformations are periodic and repeat in a distinctive way in a wide range of deformations of the sample. Deformation of the elastic-plastic composite are associated with its complex structure and studies of its mechanical properties require more advanced methods such as use of Kolmogorov-Sinai metric entropy.

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Osmęda, Anna. "Measurements of strain induced by chemical shrinkage in polymer composites." Journal of Polymer Engineering 36, no. 4 (May 1, 2016): 431–40. http://dx.doi.org/10.1515/polyeng-2015-0224.

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Abstract The aim of this work is to determine which of the techniques that allow to measure the strain induced in polymer composites by the chemical shrinkage of resin is most appropriate for predicting process-induced deformations. There are two approaches to determine the chemical strain: measurements in-plane and through-the-thickness of composite. In the following study, two methods were used for the measurement of unidirectional carbon/epoxy composite: novel one that employs a dynamic mechanical analyzer to measure through-the-thickness strain and one designed previously to measure in-plane strain. As the results of the methods were different, finite element simulation of process-induced deformation of C-sectioned composite element was carried out in order to verify the results. Comparison of numerical results with the real part deformation showed that the measurement of through-the-thickness chemical strain is the more accurate approach in the case of the prediction of deformation and that the novel method gives valid results.

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Jung, Beom-Seok, Jung-Pyo Kong, NingXue Li, Yoon-Mi Kim, Min-Saeng Kim, Sung-Hoon Ahn, and Maenghyo Cho. "Numerical simulation and verification of a curved morphing composite structure with embedded shape memory alloy wire actuators." Journal of Intelligent Material Systems and Structures 24, no. 1 (September 21, 2012): 89–98. http://dx.doi.org/10.1177/1045389x12459588.

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Shape memory alloys have been actively studied in various fields in an attempt to utilize their high energy density. In particular, shape memory alloy wire-embedded composites can be used as load-bearing smart actuators without any additional manipulation, in which they act like a hinge joint. A shape memory alloy wire-embedded composite is able to generate various deformation behaviors via the combination of its shape memory alloy and matrix materials. Accordingly, a study of the various design parameters of shape memory alloy wire-embedded composites is required to facilitate the practical application of smart structures. In this research, a numerical simulation of a shape memory alloy wire-embedded composite is used to investigate the deformation behavior of a composite panel as a function of the composite width per shape memory alloy wire, composite thickness, and the eccentricity of the shape memory alloy wire. A curved morphing composite structure is fabricated to confirm the results of the numerical simulation. The deformation of the shape memory alloy wire-embedded composite panel is determined by measuring its radius of curvature. The simulated deformation behaviors are verified with the experimental results. In addition, an analysis of the deformation and internal stress of the composites is carried out. It can be used to obtain guidelines for the mechanical design of shape memory alloy wire-embedded composite panels.

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Ивашов, А., A. Ivashov, Ю. Мандра, J. Mandra, Д. Зайцев, and D. Zaytsev. "Modelling of human teeth deformation behaviour after restoration." Actual problems in dentistry 12, no. 2 (July 26, 2016): 19–23. http://dx.doi.org/10.18481/2077-7566-2016-12-2-19-23.

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<p class="p1"><span class="s1">In the work the ef cacy of the adhesive dental restoration with different composites at monoaxial compression is tested. Deformation behavior of composite materials (SDR, Filtek P60, Filtek Ultimate Flowable, Filtek Ultimate) is compared in adhesive recording to a dentine at monoaxial compression. It is shown that mechanical properties of the composite materials are different because of their properties, but it is possible to predict their behavior in teeth after composite adhesive restoration. The highlled composites (to Filtek Ultimate and Filtek P60) are closer to dentine mechanical properties whereas the behavior of the lowlled composite materials (SDR and Filtek Ultimate Flowable) signi cantly differs from deformation behavior of a dentine. </span></p>

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Khaled, Bilal, Loukham Shyamsunder, Canio Hoffarth, Subramaniam D. Rajan, Robert K. Goldberg, Kelly S. Carney, Paul DuBois, and Gunther Blankenhorn. "Damage characterization of composites to support an orthotropic plasticity material model." Journal of Composite Materials 53, no. 7 (August 16, 2018): 941–67. http://dx.doi.org/10.1177/0021998318793506.

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The focus of this paper is the development of test procedures to characterize the damage-related behavior of a unidirectional composite at room temperature and quasi-static loading conditions and use the resulting data in the damage sub-model of a newly developed material model for orthotropic composites. This material model has three distinct sub-models to handle elastic and inelastic deformations, damage, and failure. A unidirectional composite—T800/F3900 that was the focus of our previous work, is used to illustrate how the deformation and damage-related experimental procedures are developed and used. The implementation of the damage sub-model into LS-DYNA is verified using single-element tests and validated using impact tests. Results show that the implementation yields reasonably accurate predictions of impact behavior involving deformation and damage in structural composites.

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Toubal, Lofti, Moussa Karama, and B. Lorrain. "Determination of the Matrix of Rigidity of a Composite Material by the Combination of Speckle Interferometry and Ultrasonic Measurements." Applied Mechanics and Materials 3-4 (August 2006): 155–60. http://dx.doi.org/10.4028/www.scientific.net/amm.3-4.155.

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The characterisation of composite plates used in structural work in the field of aeronautics is approached by associating ultrasound and speckle interferometry measurements. The reduced thickness of the specimens does not allow for gauge instrumentation to measure out-of plane deformation. A system was therefore used which makes it possible to obtain the cartography of the deformations in and out of-plane. This paper describes an application of electronic speckle interferometry in the measurement of through thickness deformation in composites.

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Бутенко, О. О., А. І. Місюра, Є. П. Мамуня, В. З. Барсуков, and В. Г. Хоменко. "Термомеханічний аналіз електропровідних композитних матеріалів на основі полівінілбутиралю." Bulletin of the Kyiv National University of Technologies and Design. Technical Science Series 138, no. 5 (February 3, 2020): 141–49. http://dx.doi.org/10.30857/1813-6796.2019.5.16.

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The purpose of this work was to investigate the thermomechanical properties of electrically conductive polymer composites based on polyvinylbutyral, which can be used as shielding coatings for electronic equipment. The structure of electrically conductive polymer composites was studied using a desktop scanning electron microscope (Phenom Pro ). Investigations of the temperature dependence of the deformation of composite materials were obtained using the thermomechanical analyzer Q400 EM from TA Instruments, the USA in the temperature range from 20 to 180 ° C with a heating rate of 5 ° C/min. Indentor final zone diameter was 0.85 mm, applied force was 0.28 N, which corresponds to effort of 0,5 МPа. Composites based on polymer matrix and electrically conductive carbonaceous materials with the addition of magnetite have been developed. The thermomechanical analysis of composites was shown the structural transitions of the composite over a wide temperature range. Dependences for deformation derivate vs temperature have been analized. It was established that the introduction of carbonaceous materials as filler allows increasing the value of the equilibrium modulus of composite materials in the range of plastic deformation because the fillers limit the fluidity of the composite and as result their deformation. Thermomechanical analysis of composite materials for electromagnetic shielding was performed for the first time. The influence of the deformation resistance of the material was determinate taking in the account of nature and the amount of carbonaceous materials filler in the composite. Electroconductive composite materials with high thermomechanical stability was proposed for electromagnetic shielding protection in electronic devices.

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Li, Duo Sheng, X. L. Zhou, A. H. Zou, X. Z. Hua, G. Z. Ye, and Q. J. Chen. "Study on Micro-Deformation Behavior of Sicp/Al Composites at Low Stress." Advanced Materials Research 426 (January 2012): 147–50. http://dx.doi.org/10.4028/www.scientific.net/amr.426.147.

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In this paper, SiCp/Al composites were fabricated by spontaneous infiltration technology. The micro-deformation behavior (MDB) of low tress in some silicon carbide particulate reinforced aluminum composites (SiCp/Al composites) was investigated experimentally. The microstructure, micro-deformation of samples was analyzed by OM and WDW-50 respectively. The results show that, in aluminum matrix with incorporating SiCp, the distribution of SiCp was uniform. In the same other conditions, SiCp size of the composite plays an important role on MDB at low stress, and the micro-deformation performance of the SiCp/Al composite increases with decreasing of SiCp size. MDB of composites at low stress deeply depends on the matrix material, and MDB increases with increasing of the matrix strength. It was also found that, the micro-deformation of SiCp/Al composite was negative value in the early stages of low tensile stress, and the phenomenon can be explained by strain relaxation.

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Zhou, Jinzhu, Baofu Tang, Jianfeng Zhong, Yajing Ma, and Jin Huang. "Deformation analysis and experiments for functional surface of composite antenna structure." Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science 232, no. 5 (February 17, 2017): 895–907. http://dx.doi.org/10.1177/0954406217694064.

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Composite structure with embedded microstrip antenna array is a multifunctional structure that can provide the capabilities of a panel skin structure and a radar antenna simultaneously, and it is usually installed in the structural surface of the air, water, and ground vehicles. The environmental load under in-service conditions leads to structural deformations of the composite antenna structure. In this paper, theoretical analysis and experimental validations were presented to investigate the deformations of the functional surface in the composite antenna structure. An electromechanical coupling analysis method was proposed to evaluate the performance of the deformed composite antenna structure subjected to external loads. Composite antenna structure specimens were designed, fabricated, and measured. Using the specimens, experimental systems were built to investigate the deformation. The results show that structural deformation decreases the electromagnetic performance of the composite antenna. The coupling analysis method can be applied to evaluate the performance of the deformed composite antenna structure at the design stage.

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Dissertations / Theses on the topic "Composite deformation"

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Lei, Sheng-Yuan. "Deformation micromechanics in composite structures." Thesis, University of Manchester, 2000. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.488306.

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Do, Nascimento Oliveira Jose Emidio. "Deformation and damage analysis of composite beams equipped with polyvinylidene fluoride film sensors /." [S.l. : s.n.], 2008. http://dk.cput.ac.za/cgi/viewcontent.cgi?article=1001&context=td_cput.

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Sinclair, Chad. "Co-deformation of a two-phase FCC/BCC material /." *McMaster only, 2001.

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Derian, Edward J. "Large deformation dynamic bending of composite beams." Thesis, Virginia Tech, 1985. http://hdl.handle.net/10919/45678.

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The large deformation response of composite beams subjected to a dynamic axial load was studied. The beams were loaded with a moderate amount of eccentricity to promote bending. The study was primarily experimental but some finite element results were obtained. Both the deformation and the failure of the beams were of interest. The static response of the beams was also studied in order to determine the difference between the static and dynamic failure. Twelve different laminate types were tested. The beams tested were 23 in. by 2 in. and generally 30 plies thick. The beams were loaded dynamically with a gravity-driven impactor traveling at 19.6 ft./sec. and quasi-static tests were done on identical beams in a displacement controlled manner. For laminates of practical interest, the failure modes under static and dynamic loadings were identical. Failure in most of the laminate types occurred in a single event involving 40% to 50% of the plies. However, failure in laminates with 30° or 15° off axis plies occurred in several events. All laminates exhibited bimodular properties. The compressive flexural moduli in some laminates was measured to be 1/2 the tensile flexural modulus. No simple relationship could be found among the measured ultimate failure strains of the different laminate types. Using empirically determined flexural properties, a finite element analysis was reasonably accurate in predicting the static and dynamic deformation response.

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do, Nascimento Oliveira Jose Emidio. "Deformation and damage analysis of composite beams equipped with polyvinylidene fluoride film sensors." Thesis, Cape Peninsula University of Technology, 2008. http://hdl.handle.net/20.500.11838/1284.

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In many engineering applications, it is desirable to know the behaviour of structures and systems under loading conditions. One reason is to help optimize the design and prevent damage and failure which might occur during in service and operation. Damage represents a serious problem which can cause catastrophic failure of structures, machines and systems. Therefore for safe operation, efficient and reliable methods for inspection and monitoring of damage are required. Different methods for health monitoring of structures such as non destructive testing (NDT) and strain gauges are widely used. These methods have proven to be efficient in terms of resolution and response. However, some disadvantages associated with them include the vicinity of the area under inspection which must be well known, equipment to acquire the necessary information is expensive and in many cases high skills are required for operation. On the other hand, advances in materials science and MEMS systems has promoted the use of new materials with piezoelectric properties. This include mainly polymeric and ceramic materials which after processed can be used for structural health monitoring. These materials offer a number of advantages such as lightweight, sensitivity, toughness, durability, and low cost. The present research work investigates the feasibility of using a polymeric material, Polyvinylidene Fluoride (PVDF) as a sensor for deformation and defect detection in structures. The sensors are embedded in composite cantilevered type beams to detect defects at distinct locations along the beam’s length. The defect detection method proposed is based on experimental tests and Finite Element simulations. Experimental tests on defect free and beams with manufactured internal flaws were conducted. Numerical (FEM) simulations of defect free and flawed beam models containing sections of reduced elastic modulus to represent the damage were conducted using ANSYS software. The experimental tests have been used for the validation of the numerical solution. Results have shown that the defect location changes the stiffness and indeed the frequency of vibration. For flaws near the fixed end of the beams, lower frequencies are obtained as compared to flaws away from the fixed end. PVDF sensors were used to acquire the natural frequencies of the beams for the first mode of vibration. Good agreement was verified between experimental and numerical simulation results. The work has demonstrated that PVDF film sensors can be used as possible candidates for defect detection. The analysis of the behaviour embedded PVDF sensors near the fixed end of cantilever beams, represents an initial and important step towards the application of measuring static and dynamic behaviour of structures as part of a health monitoring process.

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Bocchieri, Robert Thomas. "Time-dependent deformation of a nonlinear viscoelastic rubber-toughened fiber composite with growing damage /." Full text (PDF) from UMI/Dissertation Abstracts International, 2001. http://wwwlib.umi.com/cr/utexas/fullcit?p3008280.

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Lo, Kin Man. "Surface deformation on composite patches by constrained morphing." Thesis, University of Macau, 2010. http://umaclib3.umac.mo/record=b2493981.

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Lee, Kok Loong. "Deformation behaviour of Cu-Cr in-situ composite." Thesis, University of Leicester, 2004. http://hdl.handle.net/2381/11077.

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With the increasing requirements for higher strength materials with high electrical conductivity, a lot of interest has been paid to develop Cu-based composites in the last 25 years. These composites have superior tensile strength, combined with good electrical conductivity, to that exhibited by pure Cu and conventional Cu alloys. To date, much of the research carried out on this composite has focused on the mechanical and electrical properties of the as processed material. However, there is a basic lack of understanding of the way in which the properties may change or degrade during service. Without this knowledge, these composites cannot be fully and safely exploited. Thus the objective of this study was to investigate the thermo-mechanical behaviour of a Cu-Cr composite, and the nature and extent of any damage mechanisms occurring within the composite over a wide range of experimental conditions. Neutron diffraction was used to investigate the deformation behaviour of the individual phases in the composite and their interaction through elastic and plastic loading at room temperature. For the composite, a fairly good agreement was observed in the phase strains predicted by the Eshelby theory and measured by neutron diffraction. In-situ tensile tests in the SEM were also performed to study the damage mechanism of the composite. Tensile and creep tests were carried out in air and in vacuum over a wide range of temperatures. To provide data for comparison with the composite material, pure Cu specimens were tested whenever possible. Creep resistance increases significantly with the introduction of Cr fibres into Cu. The higher creep rate of the composite in air than in vacuum is due to the gradual decrease of the cross-sectional area of the matrix due to increasing thickness of the oxide layer. Damage characteristics and distributions were found to be similar during tensile and creep testing.

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Momken, Bahareh. "Fluid flow and deformation in composite porous media /." Full text (PDF) from UMI/Dissertation Abstracts International, 2000. http://wwwlib.umi.com/cr/utexas/fullcit?p3004343.

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Derisi, Bijan. "Development of thermoplastic composite tubes for large deformation." Thesis, Connect to online version, 2008. http://proquest.umi.com/pqdweb?did=1675143241&sid=1&Fmt=2&clientId=10306&RQT=309&VName=PQD.

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Books on the topic "Composite deformation"

1

Dvorak, George J., ed. Inelastic Deformation of Composite Materials. New York, NY: Springer New York, 1991. http://dx.doi.org/10.1007/978-1-4613-9109-8.

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2

Carper, Douglas M. Large deformation behavior of long shallow cylindrical composite panels. Hampton, Va: Langley Research Center, 1991.

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3

Sidebotham, C. Strength and deformation of composite filament wound tubes. Manchester: UMIST, 1997.

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Gol'dman, A. I͡A. Prediction of the deformation properties of polymeric and composite materials. Washington, DC: American Chemical Society, 1994.

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Gol'dman, A. I. A. Prediction of the deformation properties of polymeric and composite materials. Washington, DC: American Chemical Society, 1994.

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6

Anderson, Melvin S. Inclusion of transverse shear deformation in the exact buckling and vibration analysis of composite plate asemblies. Hampton, Va: Langley Research Center, 1993.

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7

International Conference on Deformation and Fracture of Composites (4th 1997 University of Manchester Institute of Science and Technology). 4th International Conference on Deformation and Fracture of Composites: The Manchester Conference Centre, UMIST, UK, 24-26 March 1997. [London]: Institute of Materials, 1997.

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Dvorak, George J. Inelastic Deformation of Composite Materials: IUTAM Symposium, Troy, New York, May 29 - June 1, 1990. New York, NY: Springer New York, 1991.

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9

Lim, L. G. Constitutive equations for deformation and damage in metal matrix composite materials and their application to extrusion processes. Manchester: UMIST, 1995.

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10

International Conference on Deformation and Fracture of Composites (1st 1991 University of Manchester Institute of Science and Technology). First International Conference on Deformation and Fracture of Composites: Monday-Wednesday, 25-27 March, 1991, the University of Manchester, Institute of Science and Technology, Manchester, UK. [London]: Plastics and Rubber Institute, 1991.

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Book chapters on the topic "Composite deformation"

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Shukla, Aman J., Devesh K. Chouhan, and Somjeet Biswas. "Nanostructuring of Materials by Severe Deformation Processes." In Composite Materials, 243–59. First edition. | Boca Raton, FL : CRC Press, 2021.: CRC Press, 2020. http://dx.doi.org/10.1201/9781003080633-14.

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Harik, Vasyl Michael. "Deformation of Composite Micro-Rods." In ICASE/LaRC Interdisciplinary Series in Science and Engineering, 39–58. Dordrecht: Springer Netherlands, 2004. http://dx.doi.org/10.1007/978-94-007-1013-9_2.

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Prevorsek, D. C., H. B. Chin, and Y. D. Kwon. "Deformation Analysis of Composites Exhibiting Large Strain-Rate Effects." In Composite Structures, 617–26. Dordrecht: Springer Netherlands, 1991. http://dx.doi.org/10.1007/978-94-011-3662-4_45.

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Pyrz, Ryszard. "A Hybrid Model for Nonlinear Characterization of Composite Materials." In Inelastic Deformation of Composite Materials, 695–706. New York, NY: Springer New York, 1991. http://dx.doi.org/10.1007/978-1-4613-9109-8_34.

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Hashin, Zvi. "Composite Materials with Interphase: Thermoelastic and Inelastic Effects." In Inelastic Deformation of Composite Materials, 3–34. New York, NY: Springer New York, 1991. http://dx.doi.org/10.1007/978-1-4613-9109-8_1.

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Schapery, R. A. "Simplifications in the Behavior of Viscoelastic Composites with Growing Damage." In Inelastic Deformation of Composite Materials, 193–214. New York, NY: Springer New York, 1991. http://dx.doi.org/10.1007/978-1-4613-9109-8_10.

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Castañeda, Pedro Ponte. "The Effective Properties of Brittle/Ductile Incompressible Composites." In Inelastic Deformation of Composite Materials, 215–31. New York, NY: Springer New York, 1991. http://dx.doi.org/10.1007/978-1-4613-9109-8_11.

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Fleck, N. A., and B. Budiansky. "Compressive Failure of Fibre Composites Due to Microbuckling." In Inelastic Deformation of Composite Materials, 235–73. New York, NY: Springer New York, 1991. http://dx.doi.org/10.1007/978-1-4613-9109-8_12.

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Christensen, Richard M. "A Critical Evaluation for a Class of Micro-Mechanics Models." In Inelastic Deformation of Composite Materials, 275–82. New York, NY: Springer New York, 1991. http://dx.doi.org/10.1007/978-1-4613-9109-8_13.

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Dvorak, George J., Yehia A. Bahei-El-Din, Rahul S. Shah, and Himanshu Nigam. "Experiments and Modeling in Plasticity of Fibrous Composites." In Inelastic Deformation of Composite Materials, 283–306. New York, NY: Springer New York, 1991. http://dx.doi.org/10.1007/978-1-4613-9109-8_14.

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Conference papers on the topic "Composite deformation"

1

Gardner, Leroy, Merih Kucukler, and Lorenzo Macorini. "Deformation-Based Design of Composite Beams." In International Conference on Composite Construction in Steel and Concrete 2013. Reston, VA: American Society of Civil Engineers, 2016. http://dx.doi.org/10.1061/9780784479735.011.

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KRAVCHENKO, OLEKSANDR G., SERGII G. KRAVCHENKO, and R. BYRON PIPES. "Analysis of Cure Dependent Residual Deformation in Thermosetting Composite." In American Society for Composites 2017. Lancaster, PA: DEStech Publications, Inc., 2017. http://dx.doi.org/10.12783/asc2017/15222.

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Qiu, Jinhao, Junji Tani, and Toshiyuki Takagi. "Smart composite material without thermal-bending deformation." In 1993 North American Conference on Smart Structures and Materials, edited by Vijay K. Varadan. SPIE, 1993. http://dx.doi.org/10.1117/12.148479.

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Lurie, Sergey A., Denis A. Efimov, and Natalya O. Poluhina. "Special feature of SMA composite materials deformation." In SPIE's 7th Annual International Symposium on Smart Structures and Materials, edited by Christopher S. Lynch. SPIE, 2000. http://dx.doi.org/10.1117/12.388228.

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Bahei-El-Din, Y. A., M. A. Zikry, and A. Rajendran. "Deformation Fields in Woven Composite Plates Under Impact." In ASME 2002 International Mechanical Engineering Congress and Exposition. ASMEDC, 2002. http://dx.doi.org/10.1115/imece2002-39482.

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The deformation fields and kinematics of woven composite material systems due to impact loads are analyzed and characterized for various structural parameters. Target plates comprised of woven composites with 3D preforms are considered. The analysis examines fully consolidated as well as cellular systems and simulates actual experiments. Solution of the nonlinear dynamic/contact problem was obtained by a meso-mechanics based finite element model. The results quantify experimental observations, which reveal distinct behavior under impact among nonporous and porous systems. It was found that wave propagation effects at incident energies in the order of 500 J are significant and lead to penetration at the impact face. Localized shear damage in the 3D woven system precede penetration in both the nonporous and the porous systems. The porous system is capable of dissipating more energy prior to penetration due to containment of local damage, which emanates from the void boundaries, within subsurface locations.

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Bosi, Federico, Arthur Schlothauer, Christophe Leclerc, and Sergio Pellegrino. "Cure-induced deformation of ultra-thin composite laminates." In 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-2241.

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Li, Jiuyang, and Ying Wang. "Analysis of deformation of composite wall cladding panel." In 2011 International Conference on Electrical and Control Engineering (ICECE). IEEE, 2011. http://dx.doi.org/10.1109/iceceng.2011.6058170.

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Wang, Zhiyong, Shibin Wang, Jingwei Tong, Linan Li, and C. Yue. "Measurements of interlaminar deformation in the composite laminates." In Optical Technology and Image Processing fo rFluids and solids Diagnostics 2002, edited by Gong Xin Shen, Soyoung S. Cha, Fu-Pen Chiang, and Carolyn R. Mercer. SPIE, 2003. http://dx.doi.org/10.1117/12.509773.

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Joshi, Nikhil P., and Anastasia H. Muliana. "Analyses of Deformation in Viscoelastic Sandwich Composites Subject to Moisture Diffusion." In ASME 2008 International Mechanical Engineering Congress and Exposition. ASMEDC, 2008. http://dx.doi.org/10.1115/imece2008-67006.

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Abstract:

Sandwich composites with polymer foam core are currently used in load-bearing components in buildings and naval structures due to their high strength to weight and stiffness to weight ratios, excellent thermal insulation, and ease of manufacturing. During their service time, sandwich composites are exposed to various external mechanical and hygro-thermal stimuli. It is known that the constituent properties of the sandwich composites are greatly influenced by the temperature and moisture fields. Granville [1] conducted experiments to study the effect of moisture on structural, dimensional stability, weight gain and peel strength of sandwich composites. Morganti et al. [2] analyzed the effect of moisture on the dimensional stability of the sandwich composites and concluded that moisture affects the physical behavior of the composite directly by modifying its structural characteristics such as matrix degradation and microcracks between fiber and matrix etc. However, the effect of moisture on the deformations in the sandwich composite with the viscoelastic foam cores has not yet been studied. The time-dependent response of the sandwich composite (due to the viscoelastic foam core) is aggravated in the moist environment conditions. Thus, it becomes necessary to analyze the effect of moisture on the overall response of the sandwich composites.

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Gardner, Leroy, and Xiang Yun. "Deformation based design of steel and composite structural elements." In 12th international conference on ‘Advances in Steel-Concrete Composite Structures’ - ASCCS 2018. Valencia: Universitat Politècnica València, 2018. http://dx.doi.org/10.4995/asccs2018.2018.7242.

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Abstract:

Steel and composite structures are traditionally designed through strength based calculations. An alternative approach is to consider deformation capacity. Deformation based design enables a more accurate allowance to be made for the spread of plasticity and allows strain hardening to be considered in a systematic manner. Importantly, the level of deformation required by the structure at ultimate limit state to reach the required design capacity can also be assessed. In composite construction, deformation based design enables a more rigorous assessment to be made of the development of strength in the structural system taking due account of the compatibility between the constituent materials. In this paper, recent developments to the deformation based continuous strength method for steel and composite design are described. Comparisons of capacities obtained from experiments and numerical simulations with those predicted using the continuous strength method are presented and discussed. Recommendations for future work on this topic are also set out.

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Reports on the topic "Composite deformation"

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Carter, David H. Deformation of a Beryllium-Aluminum Composite. Office of Scientific and Technical Information (OSTI), March 2000. http://dx.doi.org/10.2172/752672.

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Wiggins, Jeffrey S. Improving the Distortional Deformation Capabilities of Aerospace Composite Networks. Fort Belvoir, VA: Defense Technical Information Center, February 2011. http://dx.doi.org/10.21236/ada563649.

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Wempner, Gerald, and Wan-Lee Yin. Inelastic Deformation and Failure Analysis of Filament-Wound Composite Structures. Fort Belvoir, VA: Defense Technical Information Center, December 1988. http://dx.doi.org/10.21236/ada203382.

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Lund, T. Microstructure-strength relationship of a deformation processed aluminum-titanium composite. Office of Scientific and Technical Information (OSTI), February 1998. http://dx.doi.org/10.2172/658375.

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Xu, Kai. Microstructure-Strength Relationship of a Deformation-Processed Aluminum-Magnesium Composite. Office of Scientific and Technical Information (OSTI), September 2000. http://dx.doi.org/10.2172/764682.

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Tang, Po-Yun. Bending Deformation Increase of Bending-Extension Coupled Composite Beams Bonded with Actuator(s). Fort Belvoir, VA: Defense Technical Information Center, October 1995. http://dx.doi.org/10.21236/ada302002.

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Ren, W. Time-Dependent Deformation Modelling for a Chopped-Glass Fiber Composite for Automotive Durability Design Criteria. Office of Scientific and Technical Information (OSTI), August 2001. http://dx.doi.org/10.2172/788361.

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Dvorak, George J. Inelastic Deformation of Composite Materials. IUTAM Symposium Held in Troy, New York on May 29 - June 1, 1990. Fort Belvoir, VA: Defense Technical Information Center, January 1991. http://dx.doi.org/10.21236/ada268427.

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Bewlay, Bernard P., Melvin R. Jackson, and Clyde L. Briant. Deformation Mechanisms in Niobium Silicide-Based Composites. Fort Belvoir, VA: Defense Technical Information Center, February 2001. http://dx.doi.org/10.21236/ada387385.

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Langdon, Terence G. Processing of Metal Matrix Composites through Severe Plastic Deformation. Fort Belvoir, VA: Defense Technical Information Center, November 2003. http://dx.doi.org/10.21236/ada422186.

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