Relevant bibliographies by topics / Combustion structures

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Combustion structures'

Author: Grafiati
Published: 2 June 2025
Last updated: 31 July 2025

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Journal articles on the topic "Combustion structures"

1

Coats, C. M. "Coherent structures in combustion." Progress in Energy and Combustion Science 22, no. 5 (1996): 427–509. http://dx.doi.org/10.1016/s0360-1285(96)00011-1.

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Li, H. P. "Banded structures in unstable combustion synthesis." Journal of Materials Research 10, no. 6 (1995): 1379–86. http://dx.doi.org/10.1557/jmr.1995.1379.

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Banded structures in combustion-synthesized products have been observed during unstable combustion synthesis. The formation of the banded structures is discussed in this article. It is noted that the band spacing was changed when several initial processing conditions were varied. Any change in the processing parameters that correspondingly caused more unstable combustion was observed to decrease the propagation velocity of the combustion front and increase the band spacing. The correlation of the band spacing and oscillatory frequency of the unstable oscillatory combustion with the propagation
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Kim, Jong-Chan, Won-Chul Jung, Ji-Seok Hong, and Hong-Gye Sung. "The Effects of Turbulent Burning Velocity Models in a Swirl-Stabilized Lean Premixed Combustor." International Journal of Turbo & Jet-Engines 35, no. 4 (2018): 365–72. http://dx.doi.org/10.1515/tjj-2016-0053.

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Abstract The effects of turbulent burning velocities in a turbulent premixed combustion simulation with a G-equation are investigated using the 3D LES technique. Two turbulent burning velocity models – Kobayashi model, which takes into account the burning velocity pressure effect, and the Pitsch model, which considers the flame regions on the premixed flame structure – are implemented. An LM6000 combustor is employed to validate the turbulent premixed combustion model. The results show that the flame structures in front of the injector have different shapes in each model because of the differe
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Marudhappan, Raja, Chandrasekhar Udayagiri, and Koni Hemachandra Reddy. "Combustion chamber design and reaction modeling for aero turbo-shaft engine." Aircraft Engineering and Aerospace Technology 91, no. 1 (2018): 94–111. http://dx.doi.org/10.1108/aeat-10-2017-0217.

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Purpose The purpose of this paper is to formulate a structured approach to design an annular diffusion flame combustion chamber for use in the development of a 1,400 kW range aero turbo shaft engine. The purpose is extended to perform numerical combustion modeling by solving transient Favre Averaged Navier Stokes equations using realizable two equation k-e turbulence model and Discrete Ordinate radiation model. The presumed shape β-Probability Density Function (β-PDF) is used for turbulence chemistry interaction. The experiments are conducted on the real engine to validate the combustion chamb
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Hendricks, R. C., D. T. Shouse, W. M. Roquemore, et al. "Experimental and Computational Study of Trapped Vortex Combustor Sector Rig with High-Speed Diffuser Flow." International Journal of Rotating Machinery 7, no. 6 (2001): 375–85. http://dx.doi.org/10.1155/s1023621x0100032x.

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The Trapped Vortex Combustor (TVC) potentially offers numerous operational advantages over current production gas turbine engine combustors. These include lower weight, lower pollutant emissions, effective flame stabilization, high combustion efficiency, excellent high altitude relight capability, and operation in the lean burn or RQL modes of combustion. The present work describes the operational principles of the TVC, and extends diffuser velocities toward choked flow and provides system performance data. Performance data include EINOx results for various fuel-air ratios and combustor reside
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Meng, Nan, and Feng Li. "Large-Eddy Simulations of Unsteady Reaction Flow Characteristics Using Four Geometrical Combustor Models." Aerospace 10, no. 2 (2023): 147. http://dx.doi.org/10.3390/aerospace10020147.

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Combustion instability constitutes the primary loss source of combustion chambers, gas turbines, and aero engines, and it affects combustion performance or results in a sudden local oscillation. Therefore, this study investigated the factors affecting flame fluctuation on unsteady combustion flow fields through large-eddy simulations. The effects of primary and secondary holes in a triple swirler staged combustor on flame propagation and pressure fluctuation in a combustion field were studied. Moreover, the energy oscillations and dominant frequencies in the combustion field were obtained usin
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Zhang, Qun, Peng Zhang, Shun-li Sun, et al. "Large eddy simulation study of flow field characteristics of a combustor with two coaxial swirlers." Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy 234, no. 5 (2019): 625–42. http://dx.doi.org/10.1177/0957650919870420.

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The cold and reaction flow fields of a combustor with two coaxial swirlers are investigated by means of large eddy simulation. Effective data processing methods such as proper orthogonal decomposition and fast Fourier transform are employed for analysis. The complex flow phenomena such as swirling jet, shear layer, recirculation zone, and precession vortex core are observed and their characteristics are analyzed. The dynamics of the flame and its interactions with the complex swirling flows and large-scale eddies are characterized. The precession vortex core structures and its influences on th
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Hwang, Donghyun, Cheolwoong Kang, and Kyubok Ahn. "Effect of Mixing Section Acoustics on Combustion Instability in a Swirl-Stabilized Combustor." Energies 15, no. 22 (2022): 8492. http://dx.doi.org/10.3390/en15228492.

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An experimental study was performed to investigate the characteristics of two different combustion instability modes in a swirl-stabilized combustor. The first is the eigenfrequency corresponding to the half-wave of the combustion chamber section, and the second is the quarter-wave eigenmode of the inlet mixing section. The purpose of this study is to understand the effects of the swirl number on each combustion instability mode and analyze their generalized characteristics. Premixed gases composed of hydrocarbon fuels (C2H4 and CH4) and air were burned by independently varying the experimenta
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Peters, B. "Cellular structures in solid fuel combustion." Flow, Turbulence and Combustion 73, no. 3-4 (2005): 217–29. http://dx.doi.org/10.1007/s10494-005-4031-8.

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Arkhipov, V. A., V. N. Vilyunov, E. A. Kozlov, and Vl F. Trofimov. "Convective combustion of ordered porous structures." Combustion, Explosion, and Shock Waves 22, no. 4 (1987): 410–14. http://dx.doi.org/10.1007/bf00862882.

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Dissertations / Theses on the topic "Combustion structures"

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Atobiloye, R. Z. "Flow and combustion in vortical structures." Thesis, University of Cambridge, 1994. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.321332.

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Muhieddine, Mohamad. "Simulation numérique des structures de combustion préhistoriques." Rennes 1, 2009. ftp://ftp.irisa.fr/techreports/theses/2009/muhieddine.pdf.

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La compréhension des comportements des hommes préhistoriques nécessite la mise au point de méthodologies appropriées étudiant la nature et le fonctionnement des structures de combustion préhistoriques. Ce travail présente alors des outils numériques pour résoudre le problème de diffusion de la chaleur dans un milieu poreux saturé d'eau et pour déterminer les propriétés physiques du milieu par problème inverse. La première partie est consacrée à la résolution de problèmes de changement de phase utilisant deux approches, LHA (accumulation de chaleur latente) et AHC (capacité apparente), cette de
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Gruenert, Thomas. "Analysis of crankshaft-crankcase interaction for the prediction of the dynamic structural response and noise radiation of IC-engine structures." Thesis, Loughborough University, 2000. https://dspace.lboro.ac.uk/2134/27786.

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This thesis presents research work which is concerned with the development of analytical and numerical methods for the dynamic analysis of the crankshaft-crankcase assembly. The effects of interaction of crankshaft and crankcase on the dynamic response of an IC engine block structure are studied. These methods are especially attractive for the simulation of the steady state response of rotating systems with many degrees of freedom which are forced by multiple periodic excitations. A major novelty of the methods is the ability to model the system non-linearities successfully as frequency depend
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Kaltner, Wolfgang. "Hollow sphere structures for the emission limitation of internal combustion engines." kostenfrei, 2008. http://mediatum2.ub.tum.de/doc/650302/650302.pdf.

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Williams, Timothy C. "Combustion, NOx formation and mixing processes in Helmholtz pulse combustors." Thesis, Loughborough University, 2000. https://dspace.lboro.ac.uk/2134/18459.

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This thesis presents a laser diagnostic investigation into the combustion, NOx formation and mixing processes occurring within the optically assessed combustion chamber of a methane-fired (10kW), fully premixed, self-aspirating, Helmholtz pulse combustor. The inlet geometry of the combustion chamber consisted of a step expansion and a bluff body obstacle formed by a stagnation plate. The focus of the investigation was the effects of the stream-wise position of the stagnation plate on the pulse combustion processes. A comprehensive parametric study of the performance of the pulse combustor is p
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Albukaai, Diaa Eddin. "Les structures de combustion au Levant pendant la période Néolithique précéramique (10000-7000 BP) : typologie, techniques de construction, emplacements et fonctions." Thesis, Lyon 2, 2014. http://www.theses.fr/2014LYO20109.

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La maîtrise du feu est l’une des innovations majeures de l’histoire humaine et l'une des premières preuves de notre humanité. Le foyer est par excellence un lieu fédérateur. Son rôle social est évidemment essentiel au sein d’une population et a sans doute contribué au développement de la communication. Mais l’apport le plus important que procure le feu à l’être humain est la possibilité de cuire ses aliments, améliorant le menu quotidien de la famille préhistorique. Dans le cadre de cette recherche doctorale, les structures de combustion du Proche-Orient et plus précisément de la Syrie datant
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Kendrick, Donald William Zukoski E. E. "An experimental and numerical investigation into reacting vortex structures associated with unstable combustion /." Diss., Pasadena, Calif. : California Institute of Technology, 1995. http://resolver.caltech.edu/CaltechETD:etd-10122007-131523.

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Jarvis, Simon. "Premixed flame propagation and interaction with turbulent flow structures in a semi-confined combustion chamber." Thesis, Loughborough University, 2003. https://dspace.lboro.ac.uk/2134/10890.

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Applications of premixed turbulent combustion are common in the modern environment. The diversity of the applications spans turbulent flame propagation in explosions to combustion in an internal combustion engine. The research effort in the former is directed towards the improvement of plant safety and the latter to the reduction of harmful emissions. In this thesis key examples of the use of turbulent combustion in practical situations highlight the need for increased understanding within this field of combustion. Thus, this thesis presents a detailed laser diagnostic investigation into three
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Reveillon, Julien. "Simulation dynamique des grandes structures appliquée aux flammes turbulentes non-prémélangées." Rouen, 1996. http://www.theses.fr/1996ROUES071.

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Ce travail de thèse a été consacré à la simulation des grandes structures appliquée aux flammes turbulentes non-prémélangées. Après une étude bibliographique générale, le choix d'un modèle de sous-maille dynamique dont les paramètres s'ajustent automatiquement aux contraintes locales de l'écoulement a été effectue. La méthode de détermination des coefficients dynamiques a fait l'objet d'une attention particulière une formulation statistique, introduisant l'approche fonction densité de probabilité de sous-maille (SGPDF) a été proposée pour la modélisation de la combustion. Dans un premier temps
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Kaufman, Kelsey Leigh. "Effect of hydrogen addition and burner diameter on the stability and structure of lean, premixed flames." Thesis, University of Iowa, 2014. https://ir.uiowa.edu/etd/4661.

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Low swirl burners (LSBs) have gained popularity in heating and gas power generation industries, in part due to their proven capacity for reducing the production of NOx, which in addition to reacting to form smog and acid rain, plays a central role in the formation of the tropospheric ozone layer. With lean operating conditions, LSBs are susceptible to combustion instability, which can result in flame extinction or equipment failure. Extensive work has been performed to understand the nature of LSB combustion, but scaling trends between laboratory- and industrial-sized burners have not been est
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Books on the topic "Combustion structures"

1

Meinköhn, Dirk, ed. Dissipative Structures in Transport Processes and Combustion. Springer Berlin Heidelberg, 1990. http://dx.doi.org/10.1007/978-3-642-84230-6.

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Montserrat, Mataró i. Pladelasala, Villard Anne, and Société de recherches archéologiques de Chauvigny., eds. Les nécropoles protohistoriques et structures néolithiques: Enclos, fosses, structures de combustion. Société de recherches archéologiques, artistiques, historiques et scientifiques du Pays Chauvinois, 1993.

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Toner, S. J. Entrainment, chemistry and structures of fire plumes. U.S. Dept. of Commerce, National Bureau of Standards, Center for Fire Research, 1987.

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Meinköhn, Dirk. Dissipative Structures in Transport Processes and Combustion: Interdisciplinary Seminar, Bielefeld, July 17-21, 1989. Springer Berlin Heidelberg, 1990.

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Jacques-Pierre, Millotte, ed. Le feu domestique et ses structures au néolithique aux âges des métaux: Actes du colloque de Bourg-en-Bresse et Beaune, 7-8 octobre 2000. M. Mergoil, 2003.

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J, Maffeo Robert, Schwartz S, and United States. National Aeronautics and Space Administration., eds. Engine structures analysis software: Component specific modeling (COSMO). National Aeronautics and Space Administration, 1994.

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March, Ramiro Javier. "Méthodes physiques et chimiques appliquées à l'étude des structures de combustion préhistoriques": L'approche par la chimie organique". A.N.R.T. Université de Lille III, 1995.

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L, Berlad A., and United States. National Aeronautics and Space Administration., eds. The structure of particle cloud premixed flames. National Aeronautics and Space Administration, 1993.

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Buckmaster, John David. Flames in dusty mixtures: Their structure and stability. National Aeronautics and Space Administration, Langley Research Center, 1993.

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Merker, Günter P. Combustion Engines Development: Mixture Formation, Combustion, Emissions and Simulation. Springer-Verlag Berlin Heidelberg, 2012.

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Book chapters on the topic "Combustion structures"

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Haidn, Oskar J., Nikolaus A. Adams, Rolf Radespiel, et al. "Collaborative Research for Future Space Transportation Systems." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-53847-7_1.

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Abstract This chapter book summarizes the major achievements of the five topical focus areas, Structural Cooling, Aft-Body Flows, Combustion Chamber, Thrust Nozzle, and Thrust-Chamber Assembly of the Collaborative Research Center (Sonderforschungsbereich) Transregio 40. Obviously, only sample highlights of each of the more than twenty individual projects can be given here and thus the interested reader is invited to read their reports which again are only a summary of the entire achievements and much more information can be found in the referenced publications. The structural cooling focus are
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Chollet, J. P. "Turbulent Eddy Structures, Combustion and Chemical Reactions." In Vortex Flows and Related Numerical Methods. Springer Netherlands, 1993. http://dx.doi.org/10.1007/978-94-015-8137-0_24.

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Proctor, D., I. G. Pearson, and M. McLeod. "Co-Visualization of Flame Structures and Species." In Combustion Technologies for a Clean Environment. CRC Press, 2022. http://dx.doi.org/10.1201/9780367810597-24.

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Armbruster, Wolfgang, Justin S. Hardi, and Michael Oschwald. "Experimental Investigation of Injection-Coupled High-Frequency Combustion Instabilities." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-53847-7_16.

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Abstract Self-excited high-frequency combustion instabilities were investigated in a 42-injector cryogenic rocket combustor under representative conditions. In previous research it was found that the instabilities are connected to acoustic resonance of the shear-coaxial injectors. In order to gain a better understanding of the flame dynamics during instabilities, an optical access window was realised in the research combustor. This allowed 2D visualisation of supercritical flame response to acoustics under conditions similar to those found in European launcher engines. Through the window, high
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Ida, Tamio, and Kazutomo Ohtake. "An Experimental Study of Spatial Study and Time Resolved Structures of Turbulent Diffusion Flame." In Transport Phenomena In Combustion. Routledge, 2024. https://doi.org/10.1201/9780203735138-52.

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Dold, J. W., L. J. Hartley, and D. Green. "Dynamics of Laminar Triple-Flamelet Structures in Non-Premixed Turbulent Combustion." In Dynamical Issues in Combustion Theory. Springer New York, 1991. http://dx.doi.org/10.1007/978-1-4612-0947-8_4.

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Grossmann, S. "Turbulence and Navier-Stokes Equations." In Dissipative Structures in Transport Processes and Combustion. Springer Berlin Heidelberg, 1990. http://dx.doi.org/10.1007/978-3-642-84230-6_1.

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Bestehorn, M., and H. Haken. "Synergetics Applied to Pattern Formation in Large-Aspect-Ratio Systems." In Dissipative Structures in Transport Processes and Combustion. Springer Berlin Heidelberg, 1990. http://dx.doi.org/10.1007/978-3-642-84230-6_10.

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Klimontovich, Yu I. "Kinetic Description of Autowave Processes and Hydrodynamic Motion." In Dissipative Structures in Transport Processes and Combustion. Springer Berlin Heidelberg, 1990. http://dx.doi.org/10.1007/978-3-642-84230-6_11.

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Gray, P., and S. R. Kay. "The Non-isothermal Autocatalator: Complex Oscillations and Chaos." In Dissipative Structures in Transport Processes and Combustion. Springer Berlin Heidelberg, 1990. http://dx.doi.org/10.1007/978-3-642-84230-6_12.

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Conference papers on the topic "Combustion structures"

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Husarova, Iryna, Volodymyr Nadtoka, Maksym Kraiev, et al. "Vacuum Arc Coatings from Heat-Resistant Alloys for Combustion Chambers of Liquid-Propellant Rocket Engines." In IAF Materials and Structures Symposium, Held at the 75th International Astronautical Congress (IAC 2024). International Astronautical Federation (IAF), 2024. https://doi.org/10.52202/078369-0113.

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JOHNSTON, L., L. PERKINS, C. DENNISTON, and J. PRICE. "ADVANCED MAIN COMBUSTION CHAMBER STRUCTURAL JACKET STRENGTH ANALYSIS." In 34th Structures, Structural Dynamics and Materials Conference. American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-1395.

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Vlcek, J., H. Huber, J. Kretschmer, T. Schenkel, and H. Voggenreiter. "Spray Forming Composite Combustion Chamber Structures." In ITSC 1999, edited by E. Lugscheider and P. A. Kammer. Verlag für Schweißen und verwandte Verfahren DVS-Verlag GmbH, 1999. http://dx.doi.org/10.31399/asm.cp.itsc1999p0015.

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Abstract Atmospheric Rheo-Spraying (ARS) using the HVOF process enables injection-molded structures and thick-film coatings from steels and from high-temperature Ni-based alloys with layer thicknesses down to the centimeter. The ARS process control is based on the thermal spraying of particles in the solid state at a maximum average speed of more than 600 m/s. The coating consolidation to porosity values below 1% occurs through the particle impact with high kinetic energy. Because of the low particle oxidation, the mechanical properties of the heat-treated injection-molded structures are compa
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ALLIOT, P., A. HUCK, and P. EDLINGER. "Low cycle fatigue analysis of the combustion chamber of the Vulcain engine gas generator." In 31st Structures, Structural Dynamics and Materials Conference. American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-1045.

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Russell, Carolyn, Robert Carter, David Ellis, and Richard Goudy. "Friction Stir Welding of GR-Cop 84 for Combustion Chamber Liners." In 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference. American Institute of Aeronautics and Astronautics, 2004. http://dx.doi.org/10.2514/6.2004-1995.

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Noonan, Erin, and Mark Spearing. "Structural Design and Test of a Micro-Rocket Combustion Chamber." In 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
14th AIAA/ASME/AHS Adaptive Structures Conference
7th. American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/6.2006-1671.

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Li, Guoqiang, and Ephraim J. Gutmark. "Effects of Swirler Configurations on Flow Structures and Combustion Characteristics." In ASME Turbo Expo 2004: Power for Land, Sea, and Air. ASMEDC, 2004. http://dx.doi.org/10.1115/gt2004-53674.

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Modern gas turbine combustion technologies are driven by stringent regulations on pollutant emissions such as CO and NOx. A combustion system of multiple swirlers coupled with distributed fuel injection was studied as a new concept for reducing NOx emissions by application of Lean Direct Injection (LDI) combustion. The present paper investigates the effects of swirler configurations on the flow structures in isothermal flow and combustion cases using a multiple-swirlers fuel injector at atmospheric conditions. The swirling flow field within the combustor was characterized by a central recircul
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Shaw, Greg S., Joseph T. Snyder, Troy S. Prince, and Michael C. Willett. "A high-temperature shape memory alloy sensor for combustion monitoring and control." In Smart Structures and Materials, edited by Edward V. White. SPIE, 2005. http://dx.doi.org/10.1117/12.598051.

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Paschereit, Christian, Wolfgang Weisenstein, and Ephraim Gutmark. "Role of coherent structures in acoustic combustion control." In 29th AIAA, Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics, 1998. http://dx.doi.org/10.2514/6.1998-2433.

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Tairova, A. A., G. V. Belyakov, and S. Yu Chervinchuk. "Ablation in the slit in combustion." In PROCEEDINGS OF THE INTERNATIONAL CONFERENCE ON ADVANCED MATERIALS WITH HIERARCHICAL STRUCTURE FOR NEW TECHNOLOGIES AND RELIABLE STRUCTURES 2017 (AMHS’17). Author(s), 2017. http://dx.doi.org/10.1063/1.5013897.

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Reports on the topic "Combustion structures"

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Aggarwal, Suresh K. Spray Vaporization and Combustion in Large Vortical Structures. Defense Technical Information Center, 1997. http://dx.doi.org/10.21236/ada335808.

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McKinnon, Mark, Craig Weinschenk, and Daniel Madrzykowski. Modeling Gas Burner Fires in Ranch and Colonial Style Structures. UL Firefighter Safety Research Institute, 2020. http://dx.doi.org/10.54206/102376/mwje4818.

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The test scenarios ranged from fires in the structures with no exterior ventilation to room fires with flow paths that connected the fires with remote intake and exhaust vents. In the ranch, two replicate fires were conducted for each room of origin and each ventilation condition. Rooms of fire origin included the living room, bedroom, and kitchen. In the colonial, the focus was on varying the flow paths to examine the change in fire behavior and the resulting damage. No replicates were conducted in the colonial. After each fire scene was documented, the interior finish and furnishings were re
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Gollahalli, S. R., and N. Butuk. Combustion of pulverized coal in vortex structures. Final report, October 1, 1993--December 31, 1995. Office of Scientific and Technical Information (OSTI), 1996. http://dx.doi.org/10.2172/257349.

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Gollahalli, S. R. Combustion of pulverized coal in vortex structures. Quarterly progress report No. 7, April 1, 1995--June 30, 1995. Office of Scientific and Technical Information (OSTI), 1995. http://dx.doi.org/10.2172/137339.

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Gollahalli, S. R. Combustion of pulverized coal in vortex structures. Quarterly progress report No. 1, October 1, 1993--December 31, 1993. Office of Scientific and Technical Information (OSTI), 1994. http://dx.doi.org/10.2172/10148106.

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Gollahalli, S. R. Combustion of pulverized coal in vortex structures. Quarterly progress report No. 2, January 1, 1994--March 31, 1994. Office of Scientific and Technical Information (OSTI), 1994. http://dx.doi.org/10.2172/10153786.

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Gollahalli, S. R. Combustion of pulverized coal in vortex structures. Quarterly progress report No. 8, July 1, 1995--September 30, 1995. Office of Scientific and Technical Information (OSTI), 1995. http://dx.doi.org/10.2172/206975.

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Price, Matthew A. Effects of Cylindrical Charge Geometry and Secondary Combustion Reactions on the Internal Blast Loading of Reinforced Concrete Structures. Office of Scientific and Technical Information (OSTI), 2005. http://dx.doi.org/10.2172/841586.

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Gollahalli, S. R. Combustion of pulverized coal in vortex structures. Quarterly progress report No. 6, January 1, 1995--March 31, 1995. Office of Scientific and Technical Information (OSTI), 1995. http://dx.doi.org/10.2172/93619.

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Gollahalli, S. R. Combustion of pulverized coal in vortex structures. Quarterly progress report No. 3, April 1, 1994--June 30, 1994. Office of Scientific and Technical Information (OSTI), 1994. http://dx.doi.org/10.2172/10176380.

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