Relevant bibliographies by topics / Composite Structures

Academic literature on the topic 'Composite Structures'

Author: Grafiati
Published: 4 June 2021
Last updated: 1 August 2024

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Journal articles on the topic "Composite Structures"

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Marin, Marin, Dumitru Băleanu, and Sorin Vlase. "Composite Structures with Symmetry." Symmetry 13, no. 5 (May 3, 2021): 792. http://dx.doi.org/10.3390/sym13050792.

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In recent years, the use of composite materials in structural applications has been observed. The composites have revolutionized the field of materials and allow for interesting and new developments in different engineering branches. At the same time, in all areas of engineering, there are some products or parts of products or components that contain repetitive or identical elements. Here, different types of symmetry can occur. Such systems have been studied by various researchers in the last few decades. In civil engineering, for example, most buildings, works of art, halls, etc. have, in their structure, identical parts and symmetries. This has happened since antiquity, for different reasons. First, because of their easier, faster, and cheaper design, and second, because of their easy manufacturing and (less important for engineers, but important to the beneficiaries) for aesthetic reasons. The symmetry in the field of composite materials manifests itself in two different ways, at two levels—one due to the symmetries that appear in the composition of the composite materials and that determine the properties of the materials, and second in the structures manufactured with composites. The study of the obvious importance of the existence of symmetries in the design of composite materials or composite structures of a sandwich type, for example (but also other types), and of the existence of symmetries in structures constructed also using composite materials will be highlighted within this Special Issue. With this Issue, we want to disseminate knowledge among researchers, designers, manufacturers, and users in this exciting field.
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Abrate, Serge. "Composite structures: impact on composites 2002." Composite Structures 61, no. 1-2 (July 2003): 1. http://dx.doi.org/10.1016/s0263-8223(03)00026-6.

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Marshall, I. H. "Composite structures." NDT & E International 27, no. 4 (January 1994): 210. http://dx.doi.org/10.1016/0963-8695(94)90457-x.

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van Tooren, M., C. Kasapoglou, and H. Bersee. "Composite materials, composite structures, composite systems." Aeronautical Journal 115, no. 1174 (December 2011): 779–87. http://dx.doi.org/10.1017/s0001924000006527.

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Abstract The first part of the history of composites in aerospace emphasised materials with high specific strength and stiffness. This was followed by a quest for reliable manufacturing techniques that guaranteed sufficiently high fibre volume fractions in complex structural parts with reasonable cost. Further improvements are still possible leading, ultimately to an extension of the functionality of composite structures to non-mechanical functions. Reduction of material scatter and a more probability-based design approach, improved material properties, higher post buckling factors, improved crashworthiness concepts and improved NDI techniques are some of the evolutionary measures that could improve the performance of current composite structures. Modular design, increased co-curing, hybrid material structures, hybrid fabrication methods, innovative structural concepts and reduced development times are more revolutionary steps that could bring today’s solutions further. Manufacturing engineering is also important for achieving revolutionary change. Function integration such as embedded deicing, morphing,, and boundary-layer suction are among the next steps in weight and cost reduction, but now on the system level.
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Kientzl, Imre, Imre Norbert Orbulov, János Dobránszky, and Árpád Németh. "Mechanical Behaviour Al-Matrix Composite Wires in Double Composite Structures." Advances in Science and Technology 50 (October 2006): 147–52. http://dx.doi.org/10.4028/www.scientific.net/ast.50.147.

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The fibre reinforced metal matrix composites (FRMMC-s) are one of the main groups of the composite materials. The composite wires are continuous-fibre-reinforced aluminium matrix composites, which are made by a continuous process. Composite wires already have a few experimental applications for the reinforcement of high voltage electric cables. Other experimental application fields of these materials are the preferential reinforcement of the cast parts. In this way significant decrease in the weight could be achieved. The aim of this study is to show the excellent mechanical properties of the composite wires, and the contact relationship between the mechanical and other properties (i.e. thermoelectric power) and the possibility of their standardized production. The continuous production process of the composite wires and their test results were are shown as well. The difference between the composite wire reinforced double composite structures and direct fibre reinforced blocks were delineated as well. In this paper specimens were examined by tensile tests, bending tests, thermal aging tests and thermoelectric power measurement.
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Potter, K. D., M. R. Wisnom, M. V. Lowson, and R. D. Adams. "Innovative approaches to composite structures." Aeronautical Journal 102, no. 1012 (February 1998): 107–11. http://dx.doi.org/10.1017/s0001924000065659.

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The precise birth date of the aerospace composites industry cannot readily be identified; perhaps one should really talk about its rebirth as the first aircraft relied on natural composites such as wood. McMullen gives 1946 as the date that work on cellulose based composites for aircraft use was abandoned in favour of much more stable inorganic reinforcement fibres. This change in the direction of approach was crucial to further developments and can be thought of as marking the start of the aerospace composites industry that can be seen today. Whatever the exact date the industry is now about 50 years old so this golden jubilee edition seems an appropriate place to look at the constraints on the use of composite materials and at recent work at Bristol University aimed at reducing these constraints.
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Yu, Wenbin. "A Review of Modeling of Composite Structures." Materials 17, no. 2 (January 17, 2024): 446. http://dx.doi.org/10.3390/ma17020446.

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This paper provides a brief review on modeling of composite structures. Composite structures in this paper refer to any structure featuring anisotropy and heterogeneity, including but not limited to their traditional meaning of composite laminates made of unidirectional fiber-reinforced composites. Common methods used in modeling of composite structures, including the axiomatic method, the formal asymptotic method, and the variational asymptotic method, are illustrated in deriving the classical lamination theory for the composite laminated plates. Future research directions for modeling composite structures are also pointed out.
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Amaechi, Chiemela Victor, Cole Chesterton, Harrison Obed Butler, Nathaniel Gillet, Chunguang Wang, Idris Ahmed Ja’e, Ahmed Reda, and Agbomerie Charles Odijie. "Review of Composite Marine Risers for Deep-Water Applications: Design, Development and Mechanics." Journal of Composites Science 6, no. 3 (March 17, 2022): 96. http://dx.doi.org/10.3390/jcs6030096.

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In recent times, the utilisation of marine composites in tubular structures has grown in popularity. These applications include composite risers and related SURF (subsea umbilicals, risers and flowlines) units. The composite industry has evolved in the development of advanced composites, such as thermoplastic composite pipes (TCP) and hybrid composite structures. However, there are gaps in the understanding of its performance in composite risers, hence the need for this review on the design, hydrodynamics and mechanics of composite risers. The review covers both the structure of the composite production riser (CPR) and its end-fittings for offshore marine applications. It also reviews the mechanical behaviour of composite risers, their microstructure and strength/stress profiles. In principle, designers now have a greater grasp of composite materials. It was concluded that composites differ from standard materials such as steel. Basically, composites have weight savings and a comparative stiffness-to-strength ratio, which are advantageous in marine composites. Also, the offshore sector has grown in response to newer innovations in composite structures such as composite risers, thereby providing new cost-effective techniques. This comprehensive review shows the necessity of optimising existing designs of composite risers. Conclusions drawn portray issues facing composite riser research. Recommendations were made to encourage composite riser developments, including elaboration of necessary standards and specifications.
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McGrath, Gareth C. "Joining Composite Structures." Indian Welding Journal 33, no. 4 (October 1, 2000): 30. http://dx.doi.org/10.22486/iwj.v33i4.177842.

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Balke, Katarzyna, and Krzysztof J. Kurzydłowski. "Bridge composite structures." Mechanik, no. 7 (July 2015): 501–4. http://dx.doi.org/10.17814/mechanik.2015.7.323.

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Dissertations / Theses on the topic "Composite Structures"

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Plessas, Spyridon D. "Fluid-structure interaction in composite structures." Thesis, Monterey, California: Naval Postgraduate School, 2014. http://hdl.handle.net/10945/41432.

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In this research, dynamic characteristics of polymer composite beam and plate structures were studied when the structures were in contact with water. The effect of fluid-structure interaction (FSI) on natural frequencies, mode shapes, and dynamic responses was examined for polymer composite structures using multiphysics-based computational techniques. Composite structures were modeled using the finite element method. The fluid was modeled as an acoustic medium using the cellular automata technique. Both techniques were coupled so that both fluid and structure could interact bi-directionally. In order to make the coupling easier, the beam and plate finite elements have only displacement degrees of freedom but no rotational degrees of freedom. The fast Fourier transform (FFT) technique was applied to the transient responses of the composite structures with and without FSI, respectively, so that the effect of FSI can be examined by comparing the two results. The study showed that the effect of FSI is significant on dynamic properties of polymer composite structures. Some previous experimental observations were confirmed using the results from the computer simulations, which also enhanced understanding the effect of FSI on dynamic responses of composite structures.
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BABAEI, IMAN. "Structural Testing of Composite Crash Structures." Doctoral thesis, Politecnico di Torino, 2021. http://hdl.handle.net/11583/2910072.

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Denli, Huseyin. "Structural-acoustic optimization of composite sandwich structures." Access to citation, abstract and download form provided by ProQuest Information and Learning Company; downloadable PDF file, 168 p, 2007. http://proquest.umi.com/pqdlink?did=1251904511&Fmt=7&clientId=79356&RQT=309&VName=PQD.

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Violette, Michael A. "Fluid structure interaction effect on sandwich composite structures." Thesis, Monterey, California. Naval Postgraduate School, 2011. http://hdl.handle.net/10945/5533.

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The objective of this research is to examine the fluid structure interaction (FSI) effect on composite sandwich structures under a low velocity impact. The primary sandwich composite used in this study was a 6.35-mm balsa core and a multi-ply symmetrical plain weave 6 oz E-glass skin. The specific geometry of the composite was a 305 by 305 mm square with clamped boundary conditions. Using a uniquely designed vertical drop-weight testing machine, there were three fluid conditions in which these experiments focused. The first of these conditions was completely dry (or air) surrounded testing. The second condition was completely water submerged. The final condition was a wet top/air-backed surrounded test. The tests were conducted progressively from a low to high drop height to best conclude the onset and spread of damage to the sandwich composite when impacted with the test machine. The measured output of these tests was force levels and multi-axis strain performance. The collection and analysis of this data will help to increase the understanding of the study of sandwich composites, particularly in a marine environment.
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Daynes, Stephen. "Intelligent Responsive Composite Structures." Thesis, University of Bristol, 2010. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.520593.

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Oehlers, Deric John. "Mechanisms in composite structures /." Title page, abstract and table of contents only, 2004. http://web4.library.adelaide.edu.au/theses/09END/09endo285.pdf.

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Swanson, Gary D. "Structural efficiency study of composite wing rib structures." Thesis, This resource online, 1987. http://scholar.lib.vt.edu/theses/available/etd-04292010-020010/.

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Yang, Nana. "Structural strength and reliability analysis of composite structures." Thesis, University of Strathclyde, 2010. http://oleg.lib.strath.ac.uk:80/R/?func=dbin-jump-full&object_id=13242.

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Ullah, Israr. "Vibration-based structural health monitoring of composite structures." Thesis, University of Manchester, 2011. https://www.research.manchester.ac.uk/portal/en/theses/vibrationbased-structural-health-monitoring-of-composite-structures(f21abb03-5b46-4640-9447-0552d5e0c7d6).html.

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Composite materials are in use in several applications, for example, aircraft structural components, because of their light weight and high strength. However the delamination which is one of the serious defects often develops and propagates due to vibration during the service of the structure. The presence of this defect warrants the design life of the structure and the safety. Hence the presence of such defect has to be detected in time to plan the remedial action well in advance. There are a number of methods in the literature for damage detection. They are either 'baseline free/reference free method' or using the data from the healthy structure for damage detection. However very limited vibration-based methods are available in the literature for delamination detection in composite structures. Many of these methods are just simulated studies without experimental validation. Grossly 2 kinds of the approaches have been suggested in the literature, one related to low frequency methods and other high frequency methods. In low frequency approaches, the change in the modal parameters, curvatures, etc. is compared with the healthy structure as the reference, however in the high frequency approaches, excitation of structures at higher modes of the order of few kHz or more needed with distributed sensors to map the deflection for identification of delamination. Use of high frequency methods imposes the limitations on the use of the conventional electromagnetic shaker and vibration sensors, whereas the low frequency methods may not be feasible for practical purpose because it often requires data from the healthy state which may not be available for old structures. Hence the objective of this research is to develop a novel reference-free method which can just use the vibration responses at a few lower modes using a conventional shaker and vibration sensors (accelerometers/laser vibrometers). It is believed that the delaminated layers will interact nonlinearly when excited externally. Hence this mechanism has been utilised in the numerical simulations and the experiments on the healthy and delaminated composite plates. Two methods have been developed here - first method can quickly identify the presence of the delamination when excited at just few lower modes and other method identify the location once the presence of the delamination is confirmed. In the first approach an averaged normalised RMS has been suggested and experimentally validated for this purpose. Latter the vibration data have then been analysed further to identify the location of delamination and its size. Initially, the measured acceleration responses from the composite plates have been differentiated twice to amplify the nonlinear interaction clearly in case of delaminated plate and then kurtosis was calculated at each measured location to identify the delamination location. The method has further been simplified by just using the harmonics in the measured responses to identify the location. The thesis presents the process of the development of the novel methods, details of analysis, observations and results.
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Somanath, Nagendra. "A finite element cure model and cure cycle optimization for composite structures." Thesis, This resource online, 1987. http://scholar.lib.vt.edu/theses/available/etd-04272010-020304/.

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Books on the topic "Composite Structures"

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H, Marshall I., Scottish Development Agency, and International Conference on Composite Structures. (4th : 1987 : Paisley College of Technology, Scotland, UK), eds. Composite structures 4. London: Elsevier Applied Science, 1987.

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Reddy, J. N., and A. V. Krishna Murty, eds. Composite Structures. Berlin, Heidelberg: Springer Berlin Heidelberg, 1992. http://dx.doi.org/10.1007/978-3-662-11345-5.

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Marshall, I. H., ed. Composite Structures. Dordrecht: Springer Netherlands, 1991. http://dx.doi.org/10.1007/978-94-011-3662-4.

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Elhajjar, Rani, Peter Grant, and Cindy Ashforth. Composite Structures. Chichester, UK: John Wiley & Sons Ltd, 2018. http://dx.doi.org/10.1002/9781118997710.

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Kwon, Young W. Fluid-Structure Interaction of Composite Structures. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-57638-7.

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Marshall, I. H., ed. Composite Structures 3. Dordrecht: Springer Netherlands, 1985. http://dx.doi.org/10.1007/978-94-009-4952-2.

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Marshall, I. H., ed. Composite Structures 5. Dordrecht: Springer Netherlands, 1989. http://dx.doi.org/10.1007/978-94-009-1125-3.

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Marshall, I. H., ed. Composite Structures 4. Dordrecht: Springer Netherlands, 1987. http://dx.doi.org/10.1007/978-94-009-3455-9.

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Marshall, I. H., ed. Composite Structures 4. Dordrecht: Springer Netherlands, 1987. http://dx.doi.org/10.1007/978-94-009-3457-3.

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Kolpakov, A. G. Stressed Composite Structures. Berlin, Heidelberg: Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-540-45211-9.

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Book chapters on the topic "Composite Structures"

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Yang, Jiashi. "Composite Structures." In Analysis of Piezoelectric Semiconductor Structures, 141–76. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-48206-0_6.

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Gooch, Jan W. "Composite Structures." In Encyclopedic Dictionary of Polymers, 161. New York, NY: Springer New York, 2011. http://dx.doi.org/10.1007/978-1-4419-6247-8_2750.

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Mottram, J. Toby. "Structural Properties of a Pultruded E-Glass Fibre-Reinforced Polymeric I-Beam." In Composite Structures, 1–28. Dordrecht: Springer Netherlands, 1991. http://dx.doi.org/10.1007/978-94-011-3662-4_1.

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Hull, D., and J. C. Coppola. "Performance of Glass Fibre-Vinyl Ester Composite Tubes Crushed Using Internal Mandrels." In Composite Structures, 129–43. Dordrecht: Springer Netherlands, 1991. http://dx.doi.org/10.1007/978-94-011-3662-4_10.

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Russell, A. J., C. P. Bowers, and A. J. Moss. "Repair of Delaminations and Impact Damage in Composite Aircraft Structures." In Composite Structures, 145–59. Dordrecht: Springer Netherlands, 1991. http://dx.doi.org/10.1007/978-94-011-3662-4_11.

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Hirai, Tsuneo. "Optimization of the Design of a Filament Wound Composite Ring for Use in a Shock Absorbing System." In Composite Structures, 161–76. Dordrecht: Springer Netherlands, 1991. http://dx.doi.org/10.1007/978-94-011-3662-4_12.

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Lee, Sen Yung, Jeng Liang Jang, Jeng Sheng Lin, and Chien Jye Chou. "Hygrothermal Effects on the Linear and Nonlinear Analysis of Composite Plates." In Composite Structures, 177–86. Dordrecht: Springer Netherlands, 1991. http://dx.doi.org/10.1007/978-94-011-3662-4_13.

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Morii, Tohru, Toshio Tanimoto, Zen-Ichiro Maekawa, Hiroyuki Hamada, Atsushi Yokoyama, Kenji Kiyosumi, and Takahiro Hirano. "Effect of Water Temperature on Hygrothermal Aging of GFRP Panel." In Composite Structures, 187–201. Dordrecht: Springer Netherlands, 1991. http://dx.doi.org/10.1007/978-94-011-3662-4_14.

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Woodruff, Francis A. "Advances in Prepreg Machinery and Techniques." In Composite Structures, 203–5. Dordrecht: Springer Netherlands, 1991. http://dx.doi.org/10.1007/978-94-011-3662-4_15.

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Fang-Jing, Xu, Ye Jian-Rong, and Xue Yuan-De. "Design and Mechanical Analysis of a Hybrid Composite Driveshaft." In Composite Structures, 207–16. Dordrecht: Springer Netherlands, 1991. http://dx.doi.org/10.1007/978-94-011-3662-4_16.

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Conference papers on the topic "Composite Structures"

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FERMAN, MARTY, SALVATORE LIGUORE, CHRIS SMITH, and B. COLVIN. "COMPOSITE." In 34th Structures, Structural Dynamics and Materials Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-1341.

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Margraf, Jr., Thomas W., Thomas J. Barnell, Ernie Havens, and Christopher D. Hemmelgarn. "Reflexive composites: self-healing composite structures." In The 15th International Symposium on: Smart Structures and Materials & Nondestructive Evaluation and Health Monitoring, edited by Masayoshi Tomizuka. SPIE, 2008. http://dx.doi.org/10.1117/12.776284.

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DEMUTS, EDVINS, and PAUL SHARPE. "Tougher advanced composite structures." In 28th Structures, Structural Dynamics and Materials Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1987. http://dx.doi.org/10.2514/6.1987-794.

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PAINE, J., W. JONES, and C. ROGERS. "Nitinol actuator to host composite interfacial adhesion in adaptive hybrid composites." In 33rd Structures, Structural Dynamics and Materials Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-2405.

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Talebi, Cihan, Bülent Acar, and Gökhan O. Özgen. "Manufacturing Error Detection in Plate and Cylindrical Composite Structures." In ASME 2020 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2020. http://dx.doi.org/10.1115/imece2020-23602.

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Abstract Due to their superior weight to strength ratio of composites to common metallic structures, composite technology is widely used in aerospace industry. Assessment of damage in composites has gained interest after a large number of accidents caused by unanticipated damages in the composite structures. Many different structural health monitoring applications were developed over the years due to the fact that composite materials may inherit damage from within, not always visible from surface. The most common types of errors encountered in the industry are due to misaligned fibers, a mix-up in ply order, and delaminations: all presenting changes in the vibro-acoustical performance of the composite structure. This paper discusses the change in the dynamic properties of a composite structure contains a manufacturing error such as a ply lay-up error, and a ply angle error. Both plate and cylindrical structure types were considered for the stated error types. Effect of symmetric errors, unsymmetrical and unbalanced errors, and mid-plane errors were considered in the case of ply orientations, and dynamic stiffness matrix was used to identify the error. Identification of the structure’s layup properties and manufacturing error identification is employed. From the measured modal properties of the structure, a back-tracking strategy was used to generate the ply lay-up of the composite structure. Prepreg plates of a single carbon fiber system and filament wound hybrid cylinders consisting of glass and carbon fibers were manufactured for testing. Modal tests on plates and cylindrical composite structures were performed and compared with the analysis. A good match between the finite element model and experiment was shown in natural frequencies and mode shapes.
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Rodgers, John, and Nesbitt Hagood. "Manufacture of adaptive composite plates incorporating piezoelectric fiber composite plies." In 36th Structures, Structural Dynamics and Materials Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1995. http://dx.doi.org/10.2514/6.1995-1096.

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Chamis, Christos C. "Aerospace Composite Structures: Applications/Design/Analysis." In ASME 1998 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 1998. http://dx.doi.org/10.1115/imece1998-0386.

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Abstract Fiber composites are an emerging material with tailoring potential to achieve substantially “better-cheaper-faster” and even “greener” products. The lecture provides an overview on the advantages of composites design/analysis methods and applications. The review will synoptically cover analysis methods that span all composites scales from constituents (fiber, matrix) and fabrication process to structural optimization. Several typical composites applications to aerospace structures are presented to demonstrate specific advantages of composites in these structures. Recent application to space station, advanced satellites and X-33 are included as are potential applications of smart composite structural concepts for aerospace applications. Emerging simulation methods to evaluate the reliability and risk of aerospace composite structures are summarized. The presentation provides a broad perspective of what can be done with composites and the state of the composites technology readiness to meet even greater application challenges in aerospace structures.
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SHIAO, MICHAEL, GALIB ABUMERI, and CHRISTOS CHAMIS. "PROBABILISTIC ASSESSMENT OF COMPOSITE STRUCTURES." In 34th Structures, Structural Dynamics and Materials Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-1441.

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SHIAO, MICHAEL, and CHRISTOS CHAMIS. "PROBABILISTICALLY CONFIGURED ADAPTVE COMPOSITE STRUCTURES." In 34th Structures, Structural Dynamics and Materials Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-1679.

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Hou, An, Kurt Gramoll, An Hou, and Kurt Gramoll. "Strength of composite latticed structures." In 38th Structures, Structural Dynamics, and Materials Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1997. http://dx.doi.org/10.2514/6.1997-1251.

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Reports on the topic "Composite Structures"

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Kumar, Ashok V. Multifunctional Composite Structures. Fort Belvoir, VA: Defense Technical Information Center, March 2010. http://dx.doi.org/10.21236/ada521792.

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Garnich, Mark R., David Long, John F. Fitch, Akula M. Venkata, and Pu Liu. Precision Composite Space Structures. Fort Belvoir, VA: Defense Technical Information Center, October 2007. http://dx.doi.org/10.21236/ada472941.

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Bootle, John. High Thermal Conductivity Composite Structures. Fort Belvoir, VA: Defense Technical Information Center, October 1999. http://dx.doi.org/10.21236/ada370151.

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Bootle, John. High Thermal Conductivity Composite Structures. Fort Belvoir, VA: Defense Technical Information Center, November 1999. http://dx.doi.org/10.21236/ada379694.

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Hanson, Alexander. Revisiting Multi-Material Composite Structures with Homogenized Composite Properties. Office of Scientific and Technical Information (OSTI), January 2022. http://dx.doi.org/10.2172/1842578.

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Roach, Dennis P., Raymond Bond, and Doug Adams. Structural Health Monitoring for Impact Damage in Composite Structures. Office of Scientific and Technical Information (OSTI), August 2014. http://dx.doi.org/10.2172/1154712.

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7

Richter, Henning. Nano-composite Structures for OPV Devices. Office of Scientific and Technical Information (OSTI), November 2010. http://dx.doi.org/10.2172/993096.

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Kan, H. P., R. Cordero, and R. S. Whitehead. Advanced Certification Methodology for Composite Structures. Fort Belvoir, VA: Defense Technical Information Center, April 1997. http://dx.doi.org/10.21236/ada326762.

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Ostachowicz, W. M., M. Krawczuk, and A. Zak. Dynamics of Cracked Composite Material Structures. Fort Belvoir, VA: Defense Technical Information Center, August 1995. http://dx.doi.org/10.21236/ada303895.

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10

Dugundji, John, and Gun-Shing Chen. Dynamics and Aeroelasticity of Composite Structures. Fort Belvoir, VA: Defense Technical Information Center, March 1986. http://dx.doi.org/10.21236/ada172922.

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