Literatura académica sobre el tema "Composite materials C/C"
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Artículos de revistas sobre el tema "Composite materials C/C"
Okino, Fujio y Michiya Ota. "Nano-C/C composite materials". TANSO 2006, n.º 223 (2006): 206–14. http://dx.doi.org/10.7209/tanso.2006.206.
Texto completoKimura, Shiushichi y Eiichi Yasuda. "Carbon fiber reinforced carbon composite materials C/C composite." Bulletin of the Japan Institute of Metals 24, n.º 5 (1985): 403–9. http://dx.doi.org/10.2320/materia1962.24.403.
Texto completoAWASTHI, SHRIKANT y JERRY L. WOOD. "C/C Composite Materials for Aircraft Brakes". Advanced Ceramic Materials 3, n.º 5 (septiembre de 1988): 449–51. http://dx.doi.org/10.1111/j.1551-2916.1988.tb00254.x.
Texto completoYevtushenko, Aleksander, Michal Kuciej y Katarzyna Topczewska. "Frictional Heating during Braking of the C/C Composite Disc". Materials 13, n.º 12 (12 de junio de 2020): 2691. http://dx.doi.org/10.3390/ma13122691.
Texto completoEvdokimov, S. A., S. St Solntsev, G. V. Yermakova y D. I. Davletchin. "High-temperature protective coating for C–C composite materials". «Aviation Materials and Technologies», n.º 3 (2016): 82–87. http://dx.doi.org/10.18577/2071-9140-2016-0-3-82-87.
Texto completoZhu, Dong Mei, Hong Na Du, Fa Luo y Wan Cheng Zhou. "Preparation and Mechanical Properties of C/C-SiC Composites". Materials Science Forum 546-549 (mayo de 2007): 1501–4. http://dx.doi.org/10.4028/www.scientific.net/msf.546-549.1501.
Texto completoKim, Byung-Kook, Dong-Gap Shin, Chang-Lae Kim, Byeong-Choon Goo y Dae-Eun Kim. "Tribological Characteristics of C/C-SiC-Cu Composite and Al/SiC Composite Materials under Various Contact Conditions". Transactions of the Korean Society of Mechanical Engineers A 41, n.º 1 (1 de enero de 2017): 21–30. http://dx.doi.org/10.3795/ksme-a.2017.41.1.021.
Texto completoWielage, Bernhard, Daisy Weber, Tobias Müller y Heike Steger. "Thermo-Mechanical Monitoring of Composite Materials during the Pyrolysis of C/C Composites". Key Engineering Materials 425 (enero de 2010): 95–105. http://dx.doi.org/10.4028/www.scientific.net/kem.425.95.
Texto completoKrnel, Kristoffer, Zmago Stadler y Tomaž Kosmač. "The Influence of SiC Nano-Precipitates on the Interface Structure in C/C-SiC Composites". Advances in Science and Technology 50 (octubre de 2006): 46–50. http://dx.doi.org/10.4028/www.scientific.net/ast.50.46.
Texto completoWang, Jing, Jun Cong Wei, Chun Mei Wang y Qing Qing Zhao. "SiO/C Composite Materials for Lithium-Ion Secondary Batteries". Advanced Materials Research 750-752 (agosto de 2013): 1117–20. http://dx.doi.org/10.4028/www.scientific.net/amr.750-752.1117.
Texto completoTesis sobre el tema "Composite materials C/C"
Goettler, Christoph Michael. "EFFECT OF DENSITY ON FRICTION AND WEAR PERFORMANCE OF CARBON-CARBON COMPOSITE MATERIALS". OpenSIUC, 2020. https://opensiuc.lib.siu.edu/theses/2780.
Texto completoOzcan, Soydan. "Microstructure-property-performance relationships of c-fiber-reinforced carbon composite friction materials /". Available to subscribers only, 2008. http://proquest.umi.com/pqdweb?did=1686179081&sid=4&Fmt=2&clientId=1509&RQT=309&VName=PQD.
Texto completo"Department of Engineering Science." Keywords: Carbon composite, Friction materials, Carbon-fiber reinforcement Includes bibliographical references (p. 106-115). Also available online.
Voirin, Thibaut. "Etude du comportement mécanique et de l’endommagement des composites C/C à basses et hautes températures". Thesis, Lyon, 2021. http://www.theses.fr/2021LYSEI008.
Texto completoCarbon/Carbon composites are used in aeronautics and space industries for their excellent thermomechanical properties, from room temperature to very high temperatures (up to 3000°C). Nevertheless, these properties and their evolution at elevated temperatures are not known well enough, specifically for braking-like solicitations such as plane braking or motorsport braking.The main objectives of this work was to study the mechanical behavior of this composite under mechanical solicitations that may occur during a braking situation. Thereby, compressive and shear behavior were studied in particular, in order to determine the evolution of the damage mechanisms depending on the temperature for these loading modes. In order to lead this study successfully, various experimental aspects have been approached, such as sample geometry, as well as measurements issues due to the mechanical testing at high temperatures. This is how original mechanical testing of the interlaminar shear behavior have been performed. Concurrently with these tests, the material microstructure has been studied in-situ and post-mortem with a multi-scale approach (at ply level, at yarn level and at fiber level inside the strands). The evolution of the mechanical properties has been linked to the microstructure evolution for the different loading modes (Z-compression, XY-compression and interlaminar shear) in order to propose damage scenario of the material as a function of the temperature. This approach allowed us to understand the major role of the thermal differential dilatations of the yarn on the shrinking of the needles for temperatures up to 1500°C. For temperatures higher than 1500°C, plasticity effects have been identified
Tariq, Amna. "Design and implementation of a plasma enhanced chemical vapour deposition (PECVD) system for the study of C₆₀-polymer composite thin films and surface fuctionalization effects on C₆₀". Thesis, McGill University, 2004. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=81572.
Texto completoSen, Gupta Jayant. "Mésodynamique et rupture des composites 3D C/C sous choc : une stratégie numérique dédiée". Phd thesis, École normale supérieure de Cachan - ENS Cachan, 2005. http://tel.archives-ouvertes.fr/tel-00133772.
Texto completoKouri, Jeffrey Victor. "Improved finite element analysis of thick laminated composite plates by the predictor corrector technique and approximation of C[superscript]1 continuity with a new least squares element". Diss., Georgia Institute of Technology, 1991. http://hdl.handle.net/1853/20762.
Texto completoIqbal, Sardar S. "IMPACT OF HEAT TREATMENT AND OXIDATION OF C/C COMPOSITES ON MICROSTRUCTURE AND PHYSICAL PROPERTIES". OpenSIUC, 2011. https://opensiuc.lib.siu.edu/dissertations/430.
Texto completoDUTRA, RITA M. "Estudo da oxidação eletroquímica do etanol em meio acido utilizando os eletrocatalisadores PtSnAuRh/C e PtRuAuRh/C". reponame:Repositório Institucional do IPEN, 2016. http://repositorio.ipen.br:8080/xmlui/handle/123456789/27126.
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Os eletrocatalisadores quartenários PtSnAuRh/C e PtRuAuRh/C foram preparados nas proporções 50:40:5:5, 60:30:5:5, 70:20:5:5, 80:10:5:5, 90:4:3:3 e para as composições terciárias PtSnAu/C, PtSnRh/C, PtRuAu/C, PtRuRh/C preparados na proporção atômica 50:45:5 com (20% em massa) pelo método da redução por álcool utilizando H2PtCl6.6H2O, RuCl3·xH2O, SnCl2.2H2O, HAuCl4.3H2O e RhCl3.xH2O, como fonte de metais e carbono Vulcan XC72 como suporte e, por último, etileno glicol como agente redutor. Os eletrocatalisadores obtidos foram caracterizados fisicamente por difração de raios-X (DRX), energia dispersiva de raios X (EDX) e microscopia eletrônica de transmissão (MET). As análises por EDX mostraram que as razões atômicas dos diferentes eletrocatalisadores, preparados pelo método da redução por álcool, foram similares às composições nominais de partida indicando que esta metodologia é eficiente para a preparação destes eletrocatalisadores. Em todos os difratogramas para os eletrocatalisadores preparados observa-se um pico largo em aproximadamente 2θ = 25°, o qual é associado ao suporte de carbono e quatro outros picos de difração em aproximadamente 2θ = 40°, 47°, 67° e 82°, que por sua vez são associados aos planos (111), (200), (220) e (311), respectivamente, da estrutura cúbica de face centrada (CFC) de platina. Os resultados de difração de raios X apresentaram tamanhos médios de cristalitos entre 2,0 e 5,2 nm para PtSnAuRh/C, PtSnAu/C, PtSnRh/C e 2,0 a 2,6 nm para PtRuAuRh/C, PtRuAu/C, PtRuRh/C. Os estudos para a oxidação eletroquímica do etanol em meio ácido foram realizados utilizando as técnicas de voltametria cíclica e de cronoamperometria em uma solução 0,5 mol.L-1 H2SO4, + 1,0 mol.L-1 de C2H5OH. As curvas de polarização obtidas na célula a combustível unitária, alimentada diretamente por etanol, estão de acordo com os resultados de voltametria e cronoamperometria constatando o efeito benéfico da adição do ouro e ródio na composição dos eletrocatalisadores.
IPEN/D
Instituto de Pesquisas Energéticas e Nucleares - IPEN-CNEN/SP
Mtawa, Alexander Nikwanduka. "Influence of geometry and material properties on the optimum performance of the C-shape piezo-composite actuator". Thesis, Cape Peninsula University of Technology, 2008. http://hdl.handle.net/20.500.11838/1301.
Texto completoIn recent years, due to rapid advances in technology there has been an increasingly high demand for large displacement and large force, precise positioning, fast response, low power consuming miniature piezoelectric actuators. In certain smart structure applications, the use of curved piezoelectric actuators is necessary. The present work extends the earlier investigations on the C- shape actuator by providing a detailed investigation on the influence of geometric and material properties of the individual layers of the C-shape piezocomposite for its optimal performance as an actuator. Analytical models have. been used to optimize the geometry of the actuator. Experimental and finite element analyses (using general purpose finite element software i.e. CoventerWare and MSC. Marc) have been used for validation. The present work has established that, by maintaining the thickness of the substrate and piezoceramic layers constant; changing the external radius, for example increasing it, the stiffness of the structure decreases and thus yielding large displacement This has a negative effect on the force produced by the actuator. With fixed thickness of the substrate and varying the thickness of the piezoceramic (for fixed external radius) the result is as follows: Increasing the thickness of the piezoceramic layer has the effect of decreasing the displacement while the force increases. With fixed PZT thickness as well as the external radius, varying the substrate thickness has the following effect: As the thickness of the substrate increases the displacement increases reaching a maximum. Subsequent increase in the thickness of the substrate the displacement is reduced. The force continues increasing at least for the ratios up to 1.0, further increase of the substrate, subsequent decrease of force is also noted. In addition to changing the thickness of the substrate, the choice of different material for the substrate has the following effect: For substrate/PZT ratios of up to 0.6. an actuator with substrate material having higher elastic modulus will produce larger displacement while for ratios beyond this ratio the situation is reversed. The causes for this kind of behaviour have been addressed. In all cases both force and displacement are found to be directly proportional to applied voltage.
Chelaghma, Saber Ayoub. "Fonctionnalisation de composites C/PEKK pour application aérospatiale : caractérisation, modélisation et influence sur les propriétés du composite". Thesis, Toulouse 3, 2018. http://www.theses.fr/2018TOU30362.
Texto completoReducing aircraft weight is one of the major challenges facing the aerospace industry. In order to achieve the ambitious goals of fuel consumption and emission reduction, carbon-fiber reinforced composites have been introduced to the market. These materials are attracting increasing interest, however, they have low electrical conductivity to ensure protection against lightning strike. For this reason, composites filled with conductive particles are the subject of ongoing research activities. The objective is the development of multifunctional composites with enhanced electrical properties. Actually, the most used thermoplastic matrix is PEEK, but this polymer remains expensive, and its processing temperature is high. For this purpose, thermoplastic matrices, such as PEKK, are again studied. Between the raw material and the final part, the thermoplastic matrix undergoes several thermal steps with high temperature exposure (impregnation, consolidation, forming and assembly processes) during which its ability to crystallize evolves continuously. In order to evaluate the impact of the process and the composite constituents on its properties, crystallization has been the subject of particular attention. Two complementary experimental devices were used to characterize the crystallization. The heating stage, allows to apply a thermal cycle and observe the crystallization in optical microscopy and differential scanning calorimetry. The influence of carbon fibers and conductive fillers on the crystallization kinetics was evaluated. A decrease in crystallization times was observed through the increase of the nucleation rate. The collected data were used to develop a kinetic model identified through an original approach based on microscopic data. This model makes it possible to predict the crystallization kinetics of PEKK composites. Nevertheless, it does not make it possible to predict the final microstructure. However, the microstructure has a significant impact on mechanical properties as it has been proven through nano-indentation tests. To predict the final microstructure, a model based on the pixel coloring approach has been developed. The influence of carbon fibers has been introduced through the formation of a transcrystalline phase. A good correlation is found between the analytical approach, the simulation and the experimental data in terms of crystallization kinetics. Mechanical and electrical characterizations were performed to evaluate the performance of these new materials. On the studied materials, the mechanical response is not homogeneous as observed on tensile tests followed in stereo-correlation. The study of matter health shows the existence of defects, in particular, at the microstructure level. In order to take this particularity into account, it is thus necessary to describe the microstructure more finely. For this, X-ray tomography was used to characterize the composite. Recent developments in this technique allow, in combination with segmentation tools, to reconstruct a representative geometry of the material. This geometry is used to simulate the mechanical behaviour as well as the crystallization. The numerical simulations of an RVE are able to calculate the properties of a ply, then those of a laminate. This multi-scale modelling could reduce the number and cost of experimental campaigns. Thus, determining the properties of the final structure based on characterizations and simulation at the microstructure scale is a strategic scientific and industrial issue. This work is a contribution towards this approach
Libros sobre el tema "Composite materials C/C"
United States. National Aeronautics and Space Administration., ed. A thermally modified matrix composite material with structural integrity to 371 C. [Washington, D.C.]: National Aeronautics and Space Administration, 1988.
Buscar texto completoMinnetyan, Levon. The C(T) specimen in laminated composites testing. Cleveland, Ohio: Lewis Research Center, 1996.
Buscar texto completoSliney, Harold E. PM200, PS200: Self-lubricating bearing and seal materials for applications to 900 C. Cleveland, Ohio: Materials Division, NASA Lewis Research Center, 1991.
Buscar texto completoSliney, Harold E. PM200, PS200: Self-lubricating bearing and seal materials for applications to 900 C. Cleveland, Ohio: Materials Division, NASA Lewis Research Center, 1991.
Buscar texto completoSliney, Harold E. PM200, PS200: Self-lubricating bearing and seal materials for applications to 900 C□. Cleveland, Ohio: Materials Division, NASA Lewis Research Center, 1991.
Buscar texto completoF, Lung S., Gupta K. K y United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. A three-node C ̊element for analysis of laminated composite sandwich shells. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Buscar texto completoF, Lung S., Gupta K. K y United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. A three-node C ̊element for analysis of laminated composite sandwich shells. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Buscar texto completoStephens, Joseph R. Intermetallic and ceramic matrix composites for 815 to 1370 C (1500 to 2500 F) gas turbine engine applications. [Washington, DC]: National Aeronautics and Space Administration, 1989.
Buscar texto completoDellaCorte, Christopher. Experimentally determined wear behavior of an Al2O3-SiC composite from 25 to 1200 ̊C. [Washington, D.C.]: NASA, 1990.
Buscar texto completoDellaCorte, Christopher. Experimentally determined wear behavior of an Al2O3-SiC composite from 25 to 1200 ̊C. [Washington, D.C.]: NASA, 1990.
Buscar texto completoCapítulos de libros sobre el tema "Composite materials C/C"
Kumar, Suresh, K. Chandra Shekar, B. Jana, L. M. Manocha y N. Eswara Prasad. "C/C and C/SiC Composites for Aerospace Applications". En Aerospace Materials and Material Technologies, 343–69. Singapore: Springer Singapore, 2016. http://dx.doi.org/10.1007/978-981-10-2134-3_15.
Texto completoHou, Jun Tao, Sheng Ru Qiao, Guo Feng Lu, Cheng Yu Zhang y Yue Bing Zhang. "Internal Friction of a 2D-C/SiC Composite from 25°C to 400°C". En Key Engineering Materials, 1509–12. Stafa: Trans Tech Publications Ltd., 2007. http://dx.doi.org/10.4028/0-87849-456-1.1509.
Texto completoJi, Yong Bing, Tie Hu Li, Qi Lang Lin, Chan Ging Fang y Xiao Xian Wang. "Preparation of Mesophase Pitch from Coal Tar Pitch for C/C Composites". En Advances in Composite Materials and Structures, 165–68. Stafa: Trans Tech Publications Ltd., 2007. http://dx.doi.org/10.4028/0-87849-427-8.165.
Texto completoLi, Jian Zhang, Jun Zhang, Li Tong Zhang, Lai Fei Cheng y Yong Dong Xu. "Oxidation Behavior of Carbon Phase in 3D C/SiC Composites". En Composite Materials V, 43–47. Stafa: Trans Tech Publications Ltd., 2007. http://dx.doi.org/10.4028/0-87849-451-0.43.
Texto completoFavre, A., T. Birkel y H. Fuzellier. "Reaction between Liquid Al (or Si) and Composite C/C Materials". En High Temperature Ceramic Matrix Composites, 334–40. Weinheim, FRG: Wiley-VCH Verlag GmbH & Co. KGaA, 2006. http://dx.doi.org/10.1002/3527605622.ch53.
Texto completoLai, Zhong Hong, Jae Ho Jeon, Jing Chuan Zhu y Zhong Da Yin. "Mo-Si-C-N Multi-Layer Anti-Oxidation Coating on C/C Composites". En Key Engineering Materials, 1899–902. Stafa: Trans Tech Publications Ltd., 2007. http://dx.doi.org/10.4028/0-87849-456-1.1899.
Texto completoZhu, Dong Mei, Hong Na Du, Fa Luo y Wan Cheng Zhou. "Preparation and Mechanical Properties of C/C-SiC Composites". En Materials Science Forum, 1501–4. Stafa: Trans Tech Publications Ltd., 2007. http://dx.doi.org/10.4028/0-87849-432-4.1501.
Texto completoZhang, Fu Kuan, Yi Dong Yuan y Wan Cheng Zhou. "Research on Tribology of C/C Composites in Wet Conditions". En Materials Science Forum, 1105–8. Stafa: Trans Tech Publications Ltd., 2005. http://dx.doi.org/10.4028/0-87849-960-1.1105.
Texto completoZhu, Yun Zhou, Ming Yuan, Zheng Ren Huang, Shao Ming Dong y Dong Liang Jiang. "Effect of PCS Pyrolysis Process on C Fiber in Cf/SiC Composite". En Key Engineering Materials, 1284–86. Stafa: Trans Tech Publications Ltd., 2007. http://dx.doi.org/10.4028/0-87849-410-3.1284.
Texto completoTsuji, Nobumasa, Taiju Shibata, Junya Sumita, Masahiro Ishihara y Tatsuo Iyoku. "Study on Structural Integrity of C/C Composite Using as Core Restraint Mechanism in HTGR". En Key Engineering Materials, 2720–26. Stafa: Trans Tech Publications Ltd., 2005. http://dx.doi.org/10.4028/0-87849-978-4.2720.
Texto completoActas de conferencias sobre el tema "Composite materials C/C"
MADENCI, ERDOGAN, ATILA BARUT, AMIN YAGHOOBI, ZHIYANG YAO y YILE HU. "PERIDYNAMICS FOR MICROSTRUCTURAL DAMAGE MODELING OF 3D CARBON/CARBON (C/C) COMPOSITE MATERIALS". En Proceedings for the American Society for Composites-Thirty Eighth Technical Conference. Destech Publications, Inc., 2023. http://dx.doi.org/10.12783/asc38/36652.
Texto completoTakegoshi, Masao, Fumiei Ono, Shuichi Ueda, Toshihito Saito y Osamu Hayasaka. "Evaluation of Metallic-tube-cooled C/C Composite Structure by Rocket Combustor". En 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-2357.
Texto completoYasuda, Eiichi, Yasuhiro Tanabe y Shiushichi Kimura. "Microstructural Control and the Properties of C/C Composites". En ASME 1992 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1992. http://dx.doi.org/10.1115/92-gt-435.
Texto completoNikravan, A., H. R. Baharvandi, F. B. Jebelli, H. Abdizadeh y N. Ehsani. "Microstructure and mechanical properties of pressureless sintered B 4 C-C composite using phenolic resin". En International Conference on Smart Materials and Nanotechnology in Engineering. SPIE, 2007. http://dx.doi.org/10.1117/12.780337.
Texto completoWANG, De-Wen, Yue-Cheng YANG, Bai-Lin ZHA y Yu HU. "Study on C/C Composites Ablated in Plasma jet". En 2012 International Conference on Automobile and Traffic Science, Materials, Metallurgy Engineering (MMAT-12). Paris, France: Atlantis Press, 2013. http://dx.doi.org/10.2991/mmat.2013.42.
Texto completoDillingham, R., B. Campbell y E. Kidd. "How Advanced Composite Materials Respond to Surface Treatment". En CAMX 2019. NA SAMPE, 2019. http://dx.doi.org/10.33599/nasampe/c.19.0727.
Texto completoLeanos, Alma L. y Pavana Prabhakar. "A Novel Computational Framework for the Oxidation of C/C Composites Under Thermal Shock". En ASME 2015 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2015. http://dx.doi.org/10.1115/imece2015-51873.
Texto completoSato, Masaki, Shin-ichi Moriya, Masahiro Sato, Makoto Tadano, Kazuo Kusaka, Keiichi Hasegawa, Akinaga Kumakawa et al. "Combustion Gas Heating Tests of C∕C Composites Coated with SiC Layer". En MULTISCALE AND FUNCTIONALLY GRADED MATERIALS 2006. AIP, 2008. http://dx.doi.org/10.1063/1.2896908.
Texto completoFukushima, Noriyuki, Takenori Gomi, Samon Tanaka y Jun-ichi Matsushita. "Thermoelectric properties of SiB6-C composites". En Smart Materials and MEMS, editado por Alan R. Wilson y Hiroshi Asanuma. SPIE, 2001. http://dx.doi.org/10.1117/12.424428.
Texto completoBECKERMAN, L., T. GREENE y T. CHRISTIAN, JR. "Thermoplastic composite C-130 belly skins - Design, manufacturing, and test". En 28th Structures, Structural Dynamics and Materials Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1987. http://dx.doi.org/10.2514/6.1987-798.
Texto completoInformes sobre el tema "Composite materials C/C"
Hahn, Gail L. Accelerated Insertion of Materials - Composites (AIM-C) Methodology. Fort Belvoir, VA: Defense Technical Information Center, mayo de 2004. http://dx.doi.org/10.21236/ada511880.
Texto completoOrient, George y Gail L. Hahn. Accelerated Insertion of Materials - Composites (AIM-C). Software Component Delivery Requirements. Fort Belvoir, VA: Defense Technical Information Center, mayo de 2004. http://dx.doi.org/10.21236/ada511881.
Texto completoLease y Jones. PR-266-12213-R01 Minimizing Gas Compressor Lubricating Oil Consumption. Chantilly, Virginia: Pipeline Research Council International, Inc. (PRCI), marzo de 2013. http://dx.doi.org/10.55274/r0010085.
Texto completoBryant, C. A., S. A. Wilks y C. W. Keevil. Survival of SARS-CoV-2 on the surfaces of food and food packaging materials. Food Standards Agency, noviembre de 2022. http://dx.doi.org/10.46756/sci.fsa.kww583.
Texto completoDinh, L. y A. Saab. Isopiestic Kinetics of Powdered Pd/C/DPB Composite. Office of Scientific and Technical Information (OSTI), mayo de 2008. http://dx.doi.org/10.2172/956851.
Texto completoDinh, L., R. Meulenberg y A. Saab. Isopiestic Kinetics of Pd/C/DPB Composite: Temperature Dependence. Office of Scientific and Technical Information (OSTI), mayo de 2009. http://dx.doi.org/10.2172/956833.
Texto completoLitaor, Iggy, James Ippolito, Iris Zohar y Michael Massey. Phosphorus capture recycling and utilization for sustainable agriculture using Al/organic composite water treatment residuals. United States Department of Agriculture, enero de 2015. http://dx.doi.org/10.32747/2015.7600037.bard.
Texto completoTartakovsky, G., C. Farrow, J. McDonald, P. Allena y William Nichols. Vadose Zone Model for C-9 Pond Area for Composite Analysis. Office of Scientific and Technical Information (OSTI), septiembre de 2020. http://dx.doi.org/10.2172/1668064.
Texto completoHunten, Keith, Jon Judd, Ted Goosen, Floyd Ganus, Dennis Biddle, Glen Ziolko, Larry Karns y Sonja Baluch. PDES Application Protocol Suite for Composite (PAS-C). Functional Needs/State-Of-The-Art Comparison for the PAS-C Program. Fort Belvoir, VA: Defense Technical Information Center, mayo de 1992. http://dx.doi.org/10.21236/ada258613.
Texto completoUenal, O. Tensile and fatigue behavior of a SiC/SiC composite at 1,300 C. Office of Scientific and Technical Information (OSTI), mayo de 1996. http://dx.doi.org/10.2172/238543.
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