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Littérature scientifique sur le sujet « Composite materials Delamination »

Auteur : Grafiati
Publié le 4 juin 2021
Mis à jour le 6 septembre 2023

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Articles de revues sur le sujet "Composite materials Delamination"

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Ellison, Andrew, and Hyonny Kim. "Shadowed delamination area estimation in ultrasonic C-scans of impacted composites validated by X-ray CT." Journal of Composite Materials 54, no. 4 (July 27, 2019): 549–61. http://dx.doi.org/10.1177/0021998319865311.

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Although ultrasonic pulse-echo C-scanning is a mature non-destructive evaluation technique for imaging internal damage in composite structures, a major impediment of obtaining a full characterization of the internal damage state is delamination shadowing effects. Specifically, shadowing refers to regions of interest that are behind other delamination planes or discontinuities with respect to the scanning surface. The delamination planes block ultrasonic wave transmission and the regions of interest are thus hidden (i.e. shadowed) from the scan. A methodology has been developed to expand ultras
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Toscano, Cinzia, Aniello Riccio, FrancescoPaolo Camerlingo, and Carosena Meola. "On the use of lock-in thermography to monitor delamination growth in composite panels under compression." Science and Engineering of Composite Materials 21, no. 4 (September 1, 2014): 485–92. http://dx.doi.org/10.1515/secm-2013-0156.

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AbstractThe success of composites in automotive, aerospace, and naval applications is mainly related to their aptitude to be tailored to obtain a final product that perfectly fulfills the design requirements. However, during both manufacturing processes and maintenance, some flaws, like delaminations (which may escape simple visual inspection), may be induced in composite structures. The presence of delaminations is of major concern for the load-carrying capability of carbon fiber-reinforced polymer panels. Indeed, delaminations can strongly affect the structural strength and may grow under in
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Mahieddine, Ali, and Mohammed Ouali. "Analysis of Delaminated Composite Plates." Advanced Materials Research 686 (April 2013): 104–8. http://dx.doi.org/10.4028/www.scientific.net/amr.686.104.

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A mathematical model for plates with partially delaminated layers is presented to investigate their behavior. In this formulation account is taken of lateral strains. The principal advantage of the element is that it allows the modeling of delamination anywhere in the structure. The region without delamination is modeled to carry constant peel and shear stresses; while the region with delamination is modeled by assuming that there is no peel and shear stress transfer between the top and bottom layers. Numerical results of the present model are presented and its performance is evaluated for sta
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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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Chang, Fu-Kuo, and Zafer Kutlu. "Delamination Effects on Composite Shells." Journal of Engineering Materials and Technology 112, no. 3 (July 1, 1990): 336–40. http://dx.doi.org/10.1115/1.2903334.

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An analytical investigation was performed to study the effect of delamination on the response of cylindrical composite shells subjected to external loadings. It was of particular interest to determine the buckling load and the post-buckling behavior of externally pressurized cylindrical composite shells containing delaminations. An analytical model was developed that consists of a structural analysis for calculating the global deformations of the structures and a fracture analysis for determining the delamination growth in the structures. A nonlinear finite element code based on the updated La
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Brunner, Andreas J., René Alderliesten, and John-Alan Pascoe. "In-Service Delaminations in FRP Structures under Operational Loading Conditions: Are Current Fracture Testing and Analysis on Coupons Sufficient for Capturing the Essential Effects for Reliable Predictions?" Materials 16, no. 1 (December 27, 2022): 248. http://dx.doi.org/10.3390/ma16010248.

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Quasi-static or cyclic loading of an artificial starter crack in unidirectionally fibre-reinforced composite test coupons yields fracture mechanics data—the toughness or strain-energy release rate (labelled G)—for characterising delamination initiation and propagation. Thus far, the reproducibility of these tests is typically between 10 and 20%. However, differences in the size and possibly the shape, but also in the fibre lay-up, between test coupons and components or structures raise additional questions: Is G from a coupon test a suitable parameter for describing the behaviour of delaminati
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Subba Rao, V. V., Godavarthi Yeswanth Kiran Kumar, and Sansanka Pentapalli. "Reduction of AWJ Induced Delaminations by Impregnated Nanoclay GFRP Composites." Materials Science Forum 969 (August 2019): 284–90. http://dx.doi.org/10.4028/www.scientific.net/msf.969.284.

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Composite materials are extensively used in various applications like space, aircraft, and automobile sector because of superior physical and mechanical properties even though they are costly. In recent technological innovations, using Montmorillonite (Nanoclay) to reinforce polymer-based composites has raised attention to academic and industrial sectors since small addition could enhance Mechanical properties thereby decreasing failures like delaminations. In present research work, the effect of AWJ machining parameters on delaminations of glass fibre reinforced epoxy composite is investigate
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Wei, Z., L. H. Yam, and L. Cheng. "Delamination Assessment of Multilayer Composite Plates Using Model-based Neural Networks." Journal of Vibration and Control 11, no. 5 (May 2005): 607–25. http://dx.doi.org/10.1177/1077546305052317.

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A procedure for damage detection in multilayer composites is described using model-based neural networks and vibration response measurement. The appropriate finite element model is established to generate the training data of neural networks. Internal delaminations with different sizes and locations are considered as the particular damage scenarios in multilayer composite plates. The damage-induced energy variation of response signal is investigated, and the mechanism of mode-dependent energy dissipation of composite plates due to delamination is revealed. In order to obtain the structural dyn
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Marshall, I. H. "Delamination Buckling of Composite Materials." Composite Structures 13, no. 3 (January 1989): 235–36. http://dx.doi.org/10.1016/0263-8223(89)90007-x.

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Sreekanth, T. G., M. Senthilkumar, and S. Manikanta Reddy. "Natural Frequency based delamination estimation in GFRP beams using RSM and ANN." Frattura ed Integrità Strutturale 16, no. 61 (June 19, 2022): 487–95. http://dx.doi.org/10.3221/igf-esis.61.32.

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The importance of delamination detection can be understood from aircraft components like Vertical Stabilizer, which is subjected to heavy vibration during the flight movement and it may lead to delamination and finally even flight crash can happen because of that. Any solid structure's vibration behaviour discloses specific dynamic characteristics and property parameters of that structure. This research investigates the detection of delamination in composites using a method based on vibration signals. The composite material's flexural stiffness and strength are reduced as a result of delaminat
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Thèses sur le sujet "Composite materials Delamination"

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Whitcomb, J. D. "Instability-related delamination growth of embedded and edge delaminations." Diss., Virginia Polytechnic Institute and State University, 1988. http://hdl.handle.net/10919/77755.

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Compressive loads can cause local buckling in composite laminates that have a near-surface delamination. This buckling causes load redistribution and secondary loads, which in turn cause interlaminer stresses and delamination growth. The goal of this research effort was to enhance the understanding of this instability-related delamination growth in laminates containing either an embedded or an edge delamination. There were three primary tasks: 1) development of a geometrically nonlinear finite element analysis named NONLIN3D; 2) performance of a parametric analytical study to determine the e
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Van, Hoof J. "Modelling of impact induced delamination in composite materials." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 2000. http://www.collectionscanada.ca/obj/s4/f2/dsk1/tape4/PQDD_0028/NQ52335.pdf.

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Van, Hoof Jack (Jacobus Franciscus Adrianus Maria) Carleton University Dissertation Engineering Mechanical and Aerospace. "Modelling of impact induced delamination in composite materials." Ottawa, 1999.

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Malik, Basharat U. "Fatigue delamination growth under cyclic compression in unidirectional composites." Diss., Georgia Institute of Technology, 1995. http://hdl.handle.net/1853/12094.

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Awal, Mohammad A. 1959. "Transient response of delamination, intersecting and transverse cracks in layered composite plates." Thesis, The University of Arizona, 1989. http://hdl.handle.net/10150/276955.

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A numerical method is developed to determine the dynamic behavior of delamination and transverse cracks in multilayered plates. The plate is subjected to a time dependent antiplane shear stress field which is acting on the plate surfaces. The interaction of waves diffracted at the crack tip with those reflected at the plate boundaries and transmitted at the material interface makes the problem very complicated, so analytical study of this problem cannot be carried out with our present state of knowledge; hence the problem is solved numerically. The finite element equations are obtained by vari
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Gambone, Livio R. "The effect of R-ratio on the mode II fatigue delamination growth of unidirectional carbon/epoxy composites." Thesis, University of British Columbia, 1991. http://hdl.handle.net/2429/29968.

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An investigation of the effect of R-ratio on the mode II fatigue delamination of AS4/3501-6 carbon/epoxy composites has been undertaken. Experiments have been performed on end notched cantilever beam specimens over a wide range of R-ratios (-l ≤R ≤0.50). The measured delamination growth rate data have been correlated with the mode II values of strain energy release rate range ∆G[formula omitted]), maximum strain energy release rate (G[formula omitted]) and stress intensity factor range (∆K[formula omitted]). The growth rate is dependent on the R-ratio over the range tested. For a constant leve
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Tenek, Lazarus H. "Delamination dynamics and vibrothermographic-thermoelastic evaluation of advanced composite materials." Thesis, This resource online, 1991. http://scholar.lib.vt.edu/theses/available/etd-10312009-020116/.

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Lee, Jaehong. "Vibration, buckling and postbuckling of laminated composites with delaminations." Diss., This resource online, 1992. http://scholar.lib.vt.edu/theses/available/etd-06062008-170322/.

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Barlas, Fatma Aylin. "Variable complexity modeling of postbuckled stiffeners for delamination initiation." Thesis, This resource online, 1993. http://scholar.lib.vt.edu/theses/available/etd-10312009-020245/.

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Chang, Cherng-Chi. "Finite element analysis of laminated composite free-edge delamination specimens /." The Ohio State University, 1987. http://rave.ohiolink.edu/etdc/view?acc_num=osu1487584612162791.

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Livres sur le sujet "Composite materials Delamination"

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Kachanov, L. M. Delamination Buckling of Composite Materials. Dordrecht: Springer Netherlands, 1988. http://dx.doi.org/10.1007/978-94-009-2819-0.

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Delamination buckling of composite materials. Dordrecht: Kluwer, 1988.

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Center, Langley Research, ed. Fractography of composite delamination. Salt Lake City, Utah: University of Utah, 1990.

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Whitcomb, John David. Instability-related delamination growth of embedded and edge delaminations. Blacksburg, Va: Virginia Polytechnic Institute and State University, 1988.

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M, Newaz Golam, ed. Delamination in advanced composites. Lancaster, Pa: Technomic Pub. Co, 1991.

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J, Pagano Nicholas, ed. Interlaminar response of composite materials. Amsterdam: Elsevier, 1989.

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1954-, Newaz Golam M., ed. Delamination in advanced composites. Lancaster, Pa., U.S.A: Technomic Pub. Co., 1991.

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Institute of Materials, Minerals, and Mining, ed. Delamination behaviour of composites. Cambridge, England: Woodhead, 2008.

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United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Delamination stresses in semicircular laminated composite bars. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

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United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Delamination stresses in semicircular laminated composite bars. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

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Chapitres de livres sur le sujet "Composite materials Delamination"

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Davies, Peter, and Leif A. Carlsson. "Delamination of Composite Cylinders." In Major Accomplishments in Composite Materials and Sandwich Structures, 67–82. Dordrecht: Springer Netherlands, 2009. http://dx.doi.org/10.1007/978-90-481-3141-9_4.

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Köllner, Anton, Fabian Forsbach, and Christina Völlmecke. "Delamination Buckling in Composite Plates: an Analytical Approach to Predict Delamination Growth." In Advanced Structured Materials, 241–55. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-13307-8_18.

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Soutis, C., and S. H. Díaz Valdés. "Delamination Detection in Laminated Composites Using Lamb Waves." In Recent Advances in Composite Materials, 109–26. Dordrecht: Springer Netherlands, 2003. http://dx.doi.org/10.1007/978-94-017-2852-2_10.

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Hirwani, Chetan K., Rishabh Pal, Mrinal Chaudhury, Subrata Kumar Panda, and Nitin Sharma. "Dynamic Behavior of Laminated Composites with Internal Delamination." In Advanced Composite Materials and Structures, 277–94. Boca Raton: CRC Press, 2022. http://dx.doi.org/10.1201/9781003158813-16.

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Banks-Sills, Leslie. "Testing–Delamination Between Two Dissimilar Plies." In Interface Fracture and Delaminations in Composite Materials, 77–89. Cham: Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-60327-8_7.

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Ladeveze, P., O. Allix, and L. Daudeville. "Mesomodeling of Damage for Laminate Composites: Application to Delamination." In Inelastic Deformation of Composite Materials, 607–22. New York, NY: Springer New York, 1991. http://dx.doi.org/10.1007/978-1-4613-9109-8_29.

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Steinmetz, G., F. J. Arendts, and R. Nething. "Delamination Buckling of Laminated Plates." In Developments in the Science and Technology of Composite Materials, 495–502. Dordrecht: Springer Netherlands, 1990. http://dx.doi.org/10.1007/978-94-009-0787-4_68.

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Mróz, Z., and S. Stupkiewicz. "Hysteretic Effects and Progressive Delamination at Composite Interfaces." In IUTAM Symposium on Microstructure-Property Interactions in Composite Materials, 247–64. Dordrecht: Springer Netherlands, 1995. http://dx.doi.org/10.1007/978-94-011-0059-5_21.

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He, J., F. L. Cong, L. Lin, and B. T. Wang. "Delamination failure analysis of aircraft composite material opening siding." In Advances in Materials Science and Engineering, 623–28. London: CRC Press, 2021. http://dx.doi.org/10.1201/9781003225850-93.

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Pliusys, E., and P. T. Mativenga. "Reducing Delamination in Micro Drilling of Carbon Composite Materials." In Proceedings of the 38th International MATADOR Conference, 337–56. Cham: Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-319-64943-6_24.

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Actes de conférences sur le sujet "Composite materials Delamination"

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Johnson, Mark, and Srinivasan Sridharan. "Delamination in compressively loaded composite laminates." In 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1998. http://dx.doi.org/10.2514/6.1998-2026.

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Gu, Haozhong, and Aditi Chattopadhyay. "Delamination buckling and postbuckling of composite cylindrical shells." In 36th Structures, Structural Dynamics and Materials Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1995. http://dx.doi.org/10.2514/6.1995-1499.

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Luo, H., and S. Hanagud. "Delamination detection using dynamic characteristics of composite plates." In 36th Structures, Structural Dynamics and Materials Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1995. http://dx.doi.org/10.2514/6.1995-1172.

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Guruprasad, P. J., Ajay Kumar Tamrakar, and Dineshkumar Harursampath. "Modeling of active fiber composite for delamination sensing." In Smart Materials, Nano- and Micro-Smart Systems, edited by Nicolas H. Voelcker. SPIE, 2006. http://dx.doi.org/10.1117/12.695110.

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Chernyakin, Sergey, Sergey Perov, and Yurii Skvortsov. "Probabilistic approach at delamination propagation problem in composite materials." In ICNPAA 2018 WORLD CONGRESS: 12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences. Author(s), 2018. http://dx.doi.org/10.1063/1.5081536.

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Glaessgen, E., I. Raju, and C. Poe, Jr. "Delamination and stitch failure in stitched composite joints." In 40th Structures, Structural Dynamics, and Materials Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1999. http://dx.doi.org/10.2514/6.1999-1247.

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Zhang, Zhifang, Obinna Kenneth Ihesiulor, Krishna Shankar, and Tapabrata Ray. "Comparison of Inverse Algorithms for Delamination Detection in Composite Laminates." In ASME 2012 Conference on Smart Materials, Adaptive Structures and Intelligent Systems. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/smasis2012-7904.

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Delamination is a frequent and potentially serious damage that can occur in laminated polymer composites due to the poor inter-laminar fracture toughness of the matrix. Vibration based detection methods employ changes caused by loss of stiffness in dynamic parameters such as frequencies and mode shapes to detect and assess damage. Because it is a whole field method, and can be applied instantaneously and remotely, vibration monitoring using frequency measurements offers great potential for implementation in online structural health monitoring systems. However, one of the disadvantages of using
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Tsao, Chungchen, and Keilin Kuo. "Theoretical Analysis of Thrust-Induced Delamination in Hemispherical Drilling Composite Materials." In ASME 2014 12th Biennial Conference on Engineering Systems Design and Analysis. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/esda2014-20633.

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The theoretical analysis of thrust-induced delamination in hemispherical drilling composite materials was investigated in this study. The theoretical analysis indicated that the thrust force of hemispherical drill at drill and delamination ratio (s) about 0.8 has a significant effect on prevention of delamination damage in drilling composite materials. The maximum thrust force of hemispherical drill at α = 2, however, was about 36% of that of twist drill. In other words, hemispherical drill has a correspondence with lower bearing stresses on drilling-induced delamination, which is liable to ca
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Heidary, Hossein, Amir Refahi Oskouei, Milad Hajikhani, Behrooz Moosaloo, and Mehdi Ahmadi Najafabadi. "Acoustic Emission Signal Analysis by Wavelet Method to Investigate Damage Mechanisms During Drilling of Composite Materials." In ASME 2010 10th Biennial Conference on Engineering Systems Design and Analysis. ASMEDC, 2010. http://dx.doi.org/10.1115/esda2010-24389.

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Structural parts made of composites have frequently to be drilled in the industry. However, little is now about the interacting conditions between the drill tool and material, which may be multi-type and multi-size. Delamination free in drilling different fiber reinforced composites is the main objective of present paper. Therefore the influence of drilling and materials variables thrust force and delamination of GFRP composite was investigated experimentally. Drilling variables are cutting speed and feed; material variable is fiber orientation. Acoustic Emission sensing was employed for onlin
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Yin, Wan-Lee. "Thermal buckling of composite plates with a strip delamination." In 36th Structures, Structural Dynamics and Materials Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1995. http://dx.doi.org/10.2514/6.1995-1318.

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Rapports d'organisations sur le sujet "Composite materials Delamination"

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Bocchieri, Robert T., Douglas S. Dierdorf, Kristofor S. Cozart, Steven P. Wells, Steven W. Kirkpatrick, Robert A. MacNeill, and John R. Hawk. Experimental Investigation of Widespread Delamination Damage to Composite Materials Caused by Radiant Heating. Fort Belvoir, VA: Defense Technical Information Center, June 2013. http://dx.doi.org/10.21236/ad1009242.

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Lee, Wall, and Burch. L52333 NDE and Inspection Techniques Applied to Composite Wrap Repairs. Chantilly, Virginia: Pipeline Research Council International, Inc. (PRCI), June 2012. http://dx.doi.org/10.55274/r0010468.

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The objective includes: Assess commercially available inspection methods to validate integrity of composite repair systems. Identify applicability to inspect composite overwrap and parent metal for both onshore and sub-sea pipelines (where information is available). Identify sources of data to include other users of composite materials(aerospace/aircraft, naval/ship repairs). Identify procedures and technologies to assess inspection effectiveness and provide a gap analysis. Interface with other PRCI projects on long-term testing of composite repairs and other joint industry projects on composi
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Chin, Eric Brian, Shawn Allen English, and Timothy Briggs. Criteria for initiation of delamination in quasi-static punch-shear tests of a carbon-fiber composite material. Office of Scientific and Technical Information (OSTI), September 2015. http://dx.doi.org/10.2172/1226924.

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