Relevant bibliographies by topics / Complete combustion

Academic literature on the topic 'Complete combustion'

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Published: 4 June 2021
Last updated: 1 February 2022

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Journal articles on the topic "Complete combustion"

1

Erickson, Deborah. "Complete Combustion." Scientific American 264, no. 3 (March 1991): 113. http://dx.doi.org/10.1038/scientificamerican0391-113.

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2

Santilli, Ruggero Maria. "The Novel Hyper-Combustion for the Complete Combustion of Fossil Fuels." International Journal of Chemical Engineering and Applications 10, no. 1 (February 2019): 16–23. http://dx.doi.org/10.18178/ijcea.2019.10.1.733.

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3

Cowell, L. H., R. T. LeCren, and C. E. Tenbrook. "Two-Stage Slagging Combustor Design for a Coal-Fueled Industrial Gas Turbine." Journal of Engineering for Gas Turbines and Power 114, no. 2 (April 1, 1992): 359–66. http://dx.doi.org/10.1115/1.2906599.

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A full-size combustor for a coal-fueled industrial gas turbine engine has been designed and fabricated. The design is based on extensive work completed through one-tenth scale combustion tests. Testing of the combustion hardware will be completed with a high pressure air supply in a combustion test facility before the components are integrated with the gas turbine engine. The combustor is a two-staged, rich-lean design. Fuel and air are introduced in the primary combustion zone where the combustion process is initiated. The primary zone operates in a slagging mode inertially removing coal ash from the gas stream. Four injectors designed for coal water mixture (CWM) atomization are used to introduce the fuel and primary air. In the secondary combustion zone, additional air is injected to complete the combustion process at fuel lean conditions. The secondary zone also serves to reduce the gas temperatures exiting the combustor. Between the primary and secondary zones is a Particulate Rejection Impact Separator (PRIS). In this device much of the coal ash that passes from the primary zone is inertially separated from the gas stream. The two-staged combustor along with the PRIS have been designated as the combustor island. All of the combustor island components are refractory-lined to minimize heat loss. Fabrication of the combustor has been completed. The PRIS is still under construction. The combustor hardware is being installed at the Caterpillar Technical Center for high pressure test evaluation. The design, test installation, and test plan of the full-size combustor island are discussed.
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WANG, Rui, Xionglin LUO, and Feng XU. "Effect of CO Combustion Promoters on Combustion Air Partition in FCC under Nearly Complete Combustion." Chinese Journal of Chemical Engineering 22, no. 5 (May 2014): 531–37. http://dx.doi.org/10.1016/s1004-9541(14)60078-1.

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5

Nazhipkyzy, Meruyert, Bakytzhan Lesbayev, Gaukhar Smagulova, Ayagoz Bakkara, Zulkhair Mansurov, Nikolay Prikhodko, and Tolganay Temirgaliyeva. "Determination of complete polyethylene waste combustion mode." Chemical Bulletin of Kazakh National University, no. 2 (September 1, 2014): 93–99. http://dx.doi.org/10.15328/chemb_2014_293-99.

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6

Sakiyama, Minoru, and Tetsu Kiyobayashi. "Micro-bomb combustion calorimeter equipped with an electric heater for aiding complete combustion." Journal of Chemical Thermodynamics 32, no. 2 (February 2000): 269–79. http://dx.doi.org/10.1006/jcht.1999.0602.

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7

Zhao, Zhelong, and Xianyu Wu. "Control Oriented Model for Expander Cycle Scramjet." MATEC Web of Conferences 257 (2019): 01004. http://dx.doi.org/10.1051/matecconf/201925701004.

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As a efficient and simple design, expander cycle is widely applied in LRE engineering, but it is seldomly used on scramjet research. In order to establish a complete mathematical model for expander cycle scramjet, a control-oriented model for expander cycle scramjet is proposed in this paper. This model consists of four major parts: combustor, cooling channel, turbo pump and nozzle and gives the result of pressure, temperature, mach number and velocity distribution of combustor and cooling channel and is capable of simulate both pure supersonic combustion mode and supersonic shock wave mode of the combustor. Each part is given by specific mathematical description, which contains the calculation of airflow, combustion, heat transfer and thermal cracking of kerosene. By putting all these parts together, a complete model is formed. This model is proposed to calculate the performance and condition of the engine precisely, comprehensively, swiftly and can be directly used in further study.
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Jeong, Seung-Min, and Jeong-Yeol Choi. "Combined Diagnostic Analysis of Dynamic Combustion Characteristics in a Scramjet Engine." Energies 13, no. 15 (August 4, 2020): 4029. http://dx.doi.org/10.3390/en13154029.

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In this work, the dynamic combustion characteristics in a scramjet engine were investigated using three diagnostic data analysis methods: DMD (Dynamic Mode Decomposition), STFT (Short-Time Fourier Transform), and CEMA (Chemical Explosive Mode Analysis). The data for the analyses were obtained through a 2D numerical experiment using a DDES (Delayed Detached Eddy Simulation) turbulence model, the UCSD (University of California at San Diego) hydrogen/oxygen chemical reaction mechanism, and high-resolution schemes. The STFT was able to detect that oscillations above 50 kHz identified as dominant in FFT results were not the dominant frequencies in a channel-type combustor. In the analysis using DMD, it was confirmed that the critical point that induced a complete change of mixing characteristics existed between an injection pressure of 0.75 MPa and 1.0 MPa. A combined diagnostic analysis that included a CEMA was performed to investigate the dynamic combustion characteristics. The differences in the reaction steps forming the flame structure under each combustor condition were identified, and, through this, it was confirmed that the pressure distribution upstream of the combustor dominated the dynamic combustion characteristics of this scramjet engine. From these processes, it was confirmed that the combined analysis method used in this paper is an effective approach to diagnose the combustion characteristics of a supersonic combustor.
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Ma, Zhi Yi, Fu Lei Zhao, Ya Peng Li, Meng Lv, Le Xue, and Teng Zhang. "Analysis and Calculation of Complete Combustion Level of Biodiesel Compared with Diesel." Advanced Materials Research 512-515 (May 2012): 496–99. http://dx.doi.org/10.4028/www.scientific.net/amr.512-515.496.

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Many studies and experiments prove that biodiesel produces less CO, HC and smoke emissions, produces more NOX emission and burns more completely than diesel. Firstly, for evaluating complete combustion level for biodiesel compared with diesel, the paper indicates that heat release ratio can not act independently as the standard; secondly the second maximal heat release ratio and combustion beginning crank angles are combined with Peak heat release ratio; lastly, CAcenter(the corresponding crank angle of centric of instantaneous heat release ratio curve) is introduced and it is the best factor which can accurately reflect the complete combustion level of biodiesel.
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Li, Junhua, Huijing Fu, Lixin Fu, and Jiming Hao. "Complete Combustion of Methane over Indium Tin Oxides Catalysts." Environmental Science & Technology 40, no. 20 (October 2006): 6455–59. http://dx.doi.org/10.1021/es061629q.

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Dissertations / Theses on the topic "Complete combustion"

1

Zhu, Guanghui. "Kinetics of complete methane oxidation on palladium model catalysts." Link to electronic thesis, 2004. http://www.wpi.edu/Pubs/ETD/Available/etd-0128104-105806/.

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Thesis (Ph. D.)--Worcester Polytechnic Institute.
Keywords: deactivation; hysteresis; kinetics; structure sensitivity; methane oxidation on palladium. Includes bibliographical references (p. 150-158).
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2

de, Rooy S. C. "Improved efficiencies in flame weeding." Lincoln University, 1992. http://hdl.handle.net/10182/18.

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Possible areas of improving the efficiencies of the Lincoln University flame weeder are identified and investigated. The Hoffmann burner initially used in the Lincoln University flame weeder was found not to entrain sufficient air to allow complete combustion of the LPG used. A new burner, the Modified Lincoln University burner, was designed to improve the entrainment of air. Results show that the new design entrained sufficient air to theoretically allow complete combustion of the LPG, and this resulted in a 22.7% increase in heat output per Kg of LPG used over the Hoffmann burner. Temperature x time exposure constants required to kill weeds 0 - 15, 15 - 30, and 30 - 45 mm in size, were found to be respectively 750, 882, and 989 degrees Celsius.Seconds. These constants can be used to calculate the maximum speed of travel an operator can use a flame weeder at, once the temperature profile underneath its shields are established at various travel speeds, and therefore ensure that the flame weeder is used at its maximum efficiency. The constants can also be used to establish the cost efficiency of any flame weeder (in $/Ha), depending on the size of the weeds to be treated. The materials and methods used in establishing the temperature x time exposure constants can be used to establish the temperature x time exposure constant of any weed species at any size.
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Nguyen, Linh A. "The effect of complexes on combustion." Thesis, Aston University, 1993. http://publications.aston.ac.uk/9694/.

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The twin goals of low and efficient fuel use and minimum emissions are increasingly being addressed by research in both the motor and the catalyst industries of the world. This study was designed to attempt to investigate these goals. For diesel engine vehicles, this can be achieved by improving the efficiency of the fuel combustion in the combustion chamber. By having a suitable oxidation catalyst in the fuel one would expect the efficiency of the fuel combustion to be increased and fewer partial oxidation products to be formed. Also by placing a catalyst converter in the exhaust system partial oxidation products may be converted to more desirable final products. Finally, in this research the net catalytic effect of using an additive treated fuel and a blank ceramic monolith to trap the metal in the exhaust gases for potential use as catalytic converter was investigated. Suitable metal additives must yield a stable solution in the fuel tank. That is, they should not react with the air, water and rust that are always present. The research was targeted on the synthesis of hydrocarbon-soluble complexes that might exhibit unusually slow rates of ligand substitution. For materials containing metal ions, these properties are best met by using multi-dentate ligands that form neutral complexes. Metal complexes have been synthesised using acetylacetone derivatives, schiff base ligands and macrocyclic polyamine ligands, as potential pro-oxidant additives. Their thermal stabilities were also investigated using a differential thermal analysis instrument. The complexes were then investigated as potential additives for use in diesel fuel. The tests were conducted under controlled conditions using a diesel combustion bomb simulating the combustion process in the D.I. diesel engine, a test bed engine, and a vehicle engine.
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4

Versaevel, Philippe. "Combustion laminaire diphasique : étude théorique et expérimentale." Châtenay-Malabry, Ecole centrale de Paris, 1996. http://www.theses.fr/1996ECAP0484.

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Ce travail s’inscrit dans le cadre de recherches visant à améliorer les modèles de combustion turbulente diphasique. L’étude a consisté à analyser finement d’un point de vue théorique et expérimental la structure de deux types de flammes monodimensionnelles diphasiques laminaires : la flamme de prémélange non-étirée et la flamme de diffusion à contre-courant. Pour ces deux types de flammes, nous nous sommes attachés dans un premier à vérifier la validité de notre modélisation sur les flammes monophasiques. Grâce à une méthode originale de remaillage dynamique, des calculs en chimie complexe ont pu être réalisés sur les deux flammes diphasiques étudiées. En ce qui concerne les flammes de prémélange diphasiques, les courbes donnant la vitesse de flamme en fonction de la richesse pour différents diamètres de gouttes ont pu être obtenues numériquement, ainsi que l’extinction des flammes de prémélange riches. Les résultats obtenus sont en bon accord avec les mesures disponibles. En ce qui concerne les flammes de diffusion monophasiques, de nombreuses mesures d’extinction ont été réalisées pour différentes pressions et richesses pour valider notre code. Enfin, les limites d’extinction des flammes de diffusion diphasiques ont été obtenues numériquement en chimie complexe. Les calculs ne sont pas en bon accord avec les mesures. L’origine de ce désaccord semble provenir de la modélisation de la trainée des gouttes. Cette hypothèse est renforcée par des mesures de Vélocimétrie Laser Doppler de phase.
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Lecocq, Guillaume. "Approches hybrides combinant chimie complexe, description statistique et densité de surface de flamme pour la simulation aux grandes échelles de l'auto-inflammation, l'allumage par bougie et la flamme de prémélange dans les moteurs à allumage commandé." Phd thesis, INSA de Rouen, 2010. http://tel.archives-ouvertes.fr/tel-00561996.

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Cette thèse propose une modélisation aussi générique que possible de la combustion dans les moteurs automobiles dans un cadre de simulation aux grandes échelles. Une première étude aborde la fermeture du terme de transport non résolu pour la flamme de prémélange. Par la suite, un couplage entre les modèles ecfm-les et pcm-fpi est proposé et validé pour intégrer les effets de chimie complexe à la simulation de la flamme de prémélange. Ce travail est étendu par l'adjonction de modélisations spécifiques à l'allumage par bougie et de l'auto-inflammation, toujours en intégrant les effets de chimie détaillée. Des calculs d'application aux combustions anormales dans les moteurs à allumage commandé concluent ce travail.
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6

Meynet, Nicolas. "Simulation numérique de la combustion d'un propergol solide." Paris 6, 2005. http://www.theses.fr/2005PA066605.

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7

Bénard, Pierre. "Analyse et amélioration d'une chambre de combustion centimétrique par simulations aux grandes échelles." Thesis, Rouen, INSA, 2015. http://www.theses.fr/2015ISAM0018/document.

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Réaliser un système de combustion à petite échelle reste aujourd’hui un défi. L’augmentation du rapport surface/volume favorise les pertes thermiques, contribue à la diminution du temps de séjour et limite la turbulence. Le premier objectif de cette thèse est de comprendre les phénomènes physiques intervenant dans un brûleur centimétrique tourbillonnaire de 8 x10 x 8 mm3 (millimètre cube) et mettre au point des outils numériques adaptés. L’écoulement réactif méthane/air est étudié au moyen de simulations numériques LES. La combustion ne consomme pas l’intégralité du carburant, entraînant un rendement de combustion de l’ordre de 50% et d’importantes émissions de polluants. Le deuxième objectif est d’adapter les performances de ce brûleur. L’enrichissement en hydrogène a montré une amélioration sensible du rendement et une réduction des émissions polluantes. Plusieurs configurations géométriques de la chambre ont aussi été étudiées, ce qui a permis de dégager des axes d’améliorations
Designing a meso-scale combustion system remains a challenging scientific and technological issue. Increasing the surface-to-volume ratio promotes wall heat losses, reduces the residence time and turbulence intensity. The main objective of this thesis is to understand the physical phenomena involved in the centimetre-sized asymmetric whirl cubic burner of 8 x 10 x 8 mm3 (millimètre cube) and develop specific adapted numerical tools. The methane/air reactive flow is studied using detailed LES. While fuel and air are injected separately, combustion takes place in the premixed regime. However combustion is far from being complete, causing low combustion efficiency and significant emissions of pollutants. The second objective is to adapt in the best possible way the performances of this burner. Hydrogen enrichment of the fuel mixture showed significant efficiency enhancement and reduced pollutant emissions. Several other combustor geometries are also studied, paving the way for future improvement
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8

Ben, Dakhlia Rafik. "Combustion stationnaire et instationnaire de mélanges diphasiques." Châtenay-Malabry, Ecole centrale de Paris, 2001. http://www.theses.fr/2001ECAP0859.

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Les travaux réalisés dans cette thèse visent à améliorer la compréhension de la combustion stationnaire et instationnaire de mélanges diphasiques en prenant en compte une cinétique chimique complexe et des propriétés de transport détaillées. On présente d’abord différentes modélisations des milieux polyphasiques réactifs pour établir à partir d’un cadre cinétique une approche originale « multirayons ». Ce cadre formel est d’abord utilisé pour étudier numériquement les flammes de diffusion à contre-courant diphasiques et les flammes prémélangées planes non-étirées. Ces travaux ont permis des études paramétriques montrant d’une part que la fonction donnant l’évolution du taux de dégagement de chaleur en fonction de l’étirement est linéaire pour des flammes diphasiques, alors qu’elle suit la forme de la racine carrée de l’étirement pour les flammes gazeuses. D’autre part, des études paramétriques de flammes prémélangées diphasiques où l’on a fait varier la richesse, la fraction liquide de combustible injecté et la taille des gouttes montrent les différences importantes entre les flammes diphasiques et les flammes gazeuses. L’analyse porte ensuite sur l’évaporation d’une goutte isolée en prenant en compte l’effet Soret. On étudie l’impact de la diffusion multiespèce sur les flammes diphasiques à contre-courant et on montre que la prise en compte de l’effet Soret est nécessaire pour prédire correctement des flammes laminaires diphasiques lorsque le rapport massique combustible/diluant est important. Des simulations numériques directes de mélanges turbulents avec brouillards de gouttelettes sont ensuite effectuées et permettent de montrer que les gouttes sont rapidement convectées dans les zones où la vorticité est minimale. Cette partie doit être vue comme une première contribution à la compréhension des phénomènes instationnaires en combustion turbulente diphasique. Enfin, la dernière partie de l’étude concerne la simulation numérique directe d’une flamme prémélangée de méthanol en prenant en compte une cinétique chimique complexe et des propriétés de transport détaillées. On donne notamment une première simulation de l’interaction entre une paire de tourbillons contra-rotatifs et la flamme.
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Vincent, Stéphane. "Modélisation de l'allumage en milieu turbulent avec chimie complexe." Rouen, 1997. http://www.theses.fr/1997ROUES049.

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Ce travail concerne l'étude par simulation numérique de l'interaction qui existe entre les phénomènes turbulents et les phénomènes chimiques ayant lieu en combustion et en particulier durant les premiers instants de celle-ci. Le cas général est celui des gaz parfaitement prémélangés. Cette étude se fait par une approche basée sur les fonctions de densité de probabilité (PDF) couplée à des cinétiques chimiques complexes. Cette étude a été effectuée dans deux situations distinctes. Dans un premier temps l'étude est effectuée lorsque la combustion a lieu par auto-inflammation dans un mélange d'hydrogène et d'air a permis la mise en évidence, avec une méthode relativement simple à mettre en œuvre, des relations fortes entre les différentes espèces chimiques en cours de combustion. Ensuite cette étude a été effectuée dans le cas de l'allumage par étincelle de mélanges hydrogène-air et heptane-air en utilisant un modèle d'allumage ou l'étincelle est représentée par un dépôt d'énergie de durée finie et dans un volume fini. Le couplage de ce modèle d'allumage avec une cinétique chimique détaillée a permis la prédiction de limite d'inflammation. Le mémoire présente d'abord des rappels de la théorie de la combustion turbulente, différents types de modélisation et, en particulier, l'approche de la PDF. Puis une revue critique de modèles d'allumage par étincelle est effectuée et le modèle utilisé est présenté. Une description des méthodes de réductions des schémas numériques est proposée ainsi que le choix des cinétiques chimiques utilisées. Une étude de l'auto-allumage turbulent de mélange d'hydrogène-air est alors effectuée et dans la dernière partie l'étude de l'allumage turbulent par étincelle est effectué.
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Obounou, Marcel. "Modélisation de la combustion turbulente non prémélangée avec prise en compte d'une cinétique chimique complexe." Rouen, 1994. http://www.theses.fr/1994ROUE5011.

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Après une étude bibliographique des principaux mécanismes cinétiques globaux de la combustion du méthane, une description des modèles de combustion turbulente pour les flammes de diffusion est faite. Une amélioration du modèle lagrangien de combustion turbulente M. I. L. Est proposée à travers un calcul de délais d'ignition. Ce calcul utilise un mécanisme global de six réactions à dix espèces. Une bibliothèque de délais d'ignition est donc établie pour être utilisée dans le code de calcul Cora. Ce code utilise une méthode numérique de type différences-finies. Par ailleurs, un modèle k- standard permet de calculer les évolutions des variables dynamiques. La validation du modèle M. I. L. Avec la prise en compte d'une bibliothèque de délais d'ignition, a été faite sur une expérience de flammes de diffusion turbulente, qui présentent des zones d'extinction partielles et des zones de réallumage. Un bon accord est observé entre les calculs et les mesures des vitesses longitudinales et de l'énergie cinétique de turbulence. Le modèle k- reproduit relativement bien le champ turbulent. Les zones d'extinctions partielles et de réallumages sont retrouvées par les calculs. Tous ces résultats de calculs tendent à montrer que le modèle M. I. L. , doté d'une bibliothèque de délais d'ignition est capable de simuler de manière satisfaisante, le couplage entre la turbulence et la chimie dans les flammes turbulentes non prémélangées
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Books on the topic "Complete combustion"

1

Meincke, Mark. The complete guide to stationary gas engines. Osceola, WI, USA: Motorbooks International, 1996.

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Desideri, Umberto, Giampaolo Manfrida, and Enrico Sciubba, eds. ECOS 2012. Florence: Firenze University Press, 2012. http://dx.doi.org/10.36253/978-88-6655-322-9.

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The 8-volume set contains the Proceedings of the 25th ECOS 2012 International Conference, Perugia, Italy, June 26th to June 29th, 2012. ECOS is an acronym for Efficiency, Cost, Optimization and Simulation (of energy conversion systems and processes), summarizing the topics covered in ECOS: Thermodynamics, Heat and Mass Transfer, Exergy and Second Law Analysis, Process Integration and Heat Exchanger Networks, Fluid Dynamics and Power Plant Components, Fuel Cells, Simulation of Energy Conversion Systems, Renewable Energies, Thermo-Economic Analysis and Optimisation, Combustion, Chemical Reactors, Carbon Capture and Sequestration, Building/Urban/Complex Energy Systems, Water Desalination and Use of Water Resources, Energy Systems- Environmental and Sustainability Issues, System Operation/ Control/Diagnosis and Prognosis, Industrial Ecology.
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Vallejo Maldonado, Pablo Ramon, and Nikolay Chaynov. Kinematics and dynamics of automobile piston engines. ru: INFRA-M Academic Publishing LLC., 2019. http://dx.doi.org/10.12737/989072.

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The fundamentals of kinematics and dynamics of transport piston internal combustion engines made using different layout schemes are presented. Along with the traditional in-line, V-shaped, including oppositional, arrangement of cylinders, schemes with "staggered" arrangement of cylinders in the block at the displaced connecting rod necks of the crankshaft of the engine are considered. The kinematics of the coaxial crank mechanism is considered in detail. The questions of dynamics with reduction of calculated dependences of forces, moments, a choice of a rational order of work of cylinders in relation to the considered kinematic schemes are in detail stated. Considerable attention is paid to the unevenness of the crankshaft rotation speed and engine balancing. The loads on the main and connecting rod bearings of the crankshaft, the knowledge of which is necessary in determining the bearing capacity of bearing units, are also considered. Meets the requirements of the Federal state educational standards of higher education of the last generation. For students of higher educational institutions studying in the direction of training 23.03.03 "Operation of transport and technological machines and complexes" and related areas.
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Meincke, Mark. The Complete Guide to Stationary Gas Engines. BookSurge Publishing, 2007.

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Rogers, David R. Engine Combustion: Pressure Measurement and Analysis. 2nd ed. SAE International, 2021. http://dx.doi.org/10.4271/9781468603217.

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Engine Combustion: Pressure Measurement and Analysis, 2E provides practical information on measuring, analyzing, and qualifying combustion data, as well as details on hardware and software requirements and system components. Describing the principles of a successful combustion measurement process, the book will enable technicians and engineers to efficiently generate the required data to complete their development tasks. The revised edition has been updated with color photos and a fresh modern format has been adapted enhancing the readability of the book. As with the original printing, Engine Combustion: Pressure Measurement and Analysis, 2E is a comprehensive handbook for technicians and engineers involved in engine testing and development, and a valuable reference for scientists and students who wish to understand combustion measurement processes and techniques.
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Prior, Frederick J. b. 1858., ed. The Canadian new first, second and third year examinations for engineers and firemen: Complete explanatory and instructive answers to the three series of examination questions covering in detail locomotive firing, including combustion and care of the boiler ... Saskatoon, Sask: Western Pub. and Supply, 1996.

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Numerical solutions of the complete Navier-Stokes equations: Progress report no. 24 for the period July 1, 1993 to December 31, 1993. Raleigh, N.C: Dept. of Mechanical and Aerospace Engineering, North Carolina State University, 1994.

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United States. National Aeronautics and Space Administration., ed. Numerical solutions of the complete Navier-Stokes equations: Progress report no. 27 for the period October 1, 1995 to September 30, 1996. Raleigh, N.C: Dept. of Mechanical and Aerospace Engineering, North Carolina State University, 1996.

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Numerical solutions of the complete Navier-Stokes equations: Progress report no. 26 for the period October 1, 1994 to September 30, 1995. Raleigh, N.C: Dept. of Mechanical and Aerospace Engineering, North Carolina State University, 1995.

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United States. National Aeronautics and Space Administration., ed. Numerical solutions of the complete Navier-Stokes equations: Progress report no. 16 for the period July 1, 1998 to December 31, 1989. Raleigh, N.C: Dept. of Mechanical and Aerospace Engineering, North Carolina State University, 1989.

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Book chapters on the topic "Complete combustion"

1

Bebernes, Jerrold, and David Eberly. "The Complete Model for Solid Fuel." In Mathematical Problems from Combustion Theory, 88–106. New York, NY: Springer New York, 1989. http://dx.doi.org/10.1007/978-1-4612-4546-9_4.

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Teplitskii, Yu S., V. I. Kovenskii, and V. A. Borodulya. "Velocity of Complete Fluidization of a Polydisperse Mixture of Various Fuels." In Proceedings of the 20th International Conference on Fluidized Bed Combustion, 298–304. Berlin, Heidelberg: Springer Berlin Heidelberg, 2009. http://dx.doi.org/10.1007/978-3-642-02682-9_42.

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Chemnitz, Alexander, and Thomas Sattelmayer. "Calculation of the Thermoacoustic Stability of a Main Stage Thrust Chamber Demonstrator." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 235–47. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-53847-7_15.

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Abstract The stability behavior of a virtual thrust chamber demonstrator with low injection pressure loss is studied numerically. The approach relies on an eigenvalue analysis of the Linearized Euler Equations. An updated form of the stability prediction procedure is outlined, addressing mean flow and flame response calculations. The acoustics of the isolated oxidizer dome are discussed as well as the complete system incorporating dome and combustion chamber. The coupling between both components is realized via a scattering matrix representing the injectors. A flame transfer function is applied to determine the damping rates. Thereby it is found that the procedure for the extraction of the flame transfer function from the CFD solution has a significant impact on the stability predictions.
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Olmeda, R., P. Breda, C. Stemmer, and M. Pfitzner. "Large-Eddy Simulations for the Wall Heat Flux Prediction of a Film-Cooled Single-Element Combustion Chamber." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 223–34. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-53847-7_14.

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Abstract In order for modern launcher engines to work at their optimum, film cooling can be used to preserve the structural integrity of the combustion chamber. The analysis of this cooling system by means of CFD is complex due to the extreme physical conditions and effects like turbulent fluctuations damping and recombination processes in the boundary layer which locally change the transport properties of the fluid. The combustion phenomena are modeled by means of Flamelet tables taking into account the enthalpy loss in the proximity of the chamber walls. In this work, Large-Eddy Simulations of a single-element combustion chamber experimentally investigated at the Technical University of Munich are carried out at cooled and non-cooled conditions. Compared with the experiment, the LES shows improved results with respect to RANS simulations published. The influence of wall roughness on the wall heat flux is also studied, as it plays an important role for the lifespan of a rocket engine combustors.
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Yu, Jun, Laura K. Gross, and Christopher M. Danforth. "Complex dynamic behavior on transition in a solid combustion model." In Unifying Themes in Complex Systems, 339–46. Berlin, Heidelberg: Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-540-85081-6_43.

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Finney, Charles E. A., Miroslav K. Stoyanov, Sreekanth Pannala, C. Stuart Daw, Robert M. Wagner, K. Dean Edwards, Clayton G. Webster, and Johney B. Green. "Application of High Performance Computing for Simulating the Unstable Dynamics of Dilute Spark-Ignited Combustion." In Understanding Complex Systems, 259–70. Cham: Springer International Publishing, 2013. http://dx.doi.org/10.1007/978-3-319-02925-2_23.

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Mumford, Judy L., Robert S. Chapman, Stephen Nesnow, C. Tuker Helmes, and Xueming Li. "Mutagenicity, Carcinogenicity, and Human Cancer Risk from Indoor Exposure to Coal and Wood Combustion in Xuan Wei, China." In Genetic Toxicology of Complex Mixtures, 157–63. Boston, MA: Springer US, 1990. http://dx.doi.org/10.1007/978-1-4684-5850-3_12.

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Grimmer, G., H. Brune, G. Dettbarn, J. Jacob, J. Misfeld, U. Mohr, K. W. Naujack, J. Timm, and R. Wenzel-Hartung. "Contribution of Polycyclic Aromatic Hydrocarbons and Other Polycyclic Aromatic Compounds to the Carcinogenicity of Combustion Source and Air Pollution." In Genetic Toxicology of Complex Mixtures, 127–40. Boston, MA: Springer US, 1991. http://dx.doi.org/10.1007/978-1-4684-5850-3_9.

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Atkins, Peter. "Burns Night: Combustion." In Reactions. Oxford University Press, 2011. http://dx.doi.org/10.1093/oso/9780199695126.003.0007.

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Burning, more formally combustion, denotes burning in oxygen and more commonly in air (which is 20 per cent oxygen). Combustion is a special case of a more general term, ‘oxidation’, which originally meant reaction with oxygen, not necessarily accompanied by a flame. The rusting of iron is also an oxidation, but we don’t normally think of it as a combustion because no flame is involved. Oxidation now has a much broader meaning than reaction with oxygen, as I shall unfold in Reaction 5. For now, I shall stick to combustion itself. To achieve combustion, we take a fuel, which might be the methane, CH4, 1, of natural gas or one of the heavier hydrocarbons, such as octane, C8H18, 2, that we use in internal combustion engines, mix it with air, and ignite it. The outcome of the complete combustion of any hydro-carbon is carbon dioxide and water but incomplete combustion can result in carbon monoxide and various fragments of the original hydrocarbon molecule. All combustions are ‘exothermic’, meaning that they release a lot of energy as heat into the surroundings. We use that energy for warmth or for driving machinery. Another example of an exothermic combustion is provided by the metal magnesium, which gives an intense white light as well as heat when it burns in air. A part of the vigour of this reaction is due to the fact that magnesium reacts not only with oxygen but also with nitrogen, the major component of air. You should be getting a glimpse of the broader significance of the term ‘oxidation’ in the sense that the reaction need not involve oxygen; in magnesium’s case, nitrogen can replace oxygen in the reaction. Magnesium foil was used in old-fashioned photographic flashes and in fireworks. The latter now mostly use finely powdered aluminium, which is much cheaper than magnesium and reacts in much the same way. In what follows you could easily replace aluminium with magnesium if you want to think fireworks. For the whole of the following discussion you need to be familiar with oxygen, O2, 3, a peculiar molecule in several respects.
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Petryshyn, Igor, and Olexandr Bas. "NATURAL GAS HEAT COMBUSTION DETERMINATION ON MEASURING SYSTEMS WITH DUPLICATE GAS UNITS." In Integration of traditional and innovative scientific researches: global trends and regional aspect. Publishing House “Baltija Publishing”, 2020. http://dx.doi.org/10.30525/978-9934-26-001-8-2-8.

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The paper focuses on the need to determine the natural gas heat combustion in order to transition to gas metering in units of energy. The technical organization of gas transportation in the main and distribution pipelines on the territory of Ukraine is shown. A detailed analysis of regulatory and legal support, which regulates the definition and accounting of quantitative and qualitative characteristics of natural gas at gas metering units. The draft Rules for determining the natural gas volume are considered in detail. Specified variants of determining the weighted average value of combustion heat in the case of complex gas supply systems with the use of flow measuring means of gas combustion heat. The necessity and urgency of determining the natural gas heat combustion on measuring systems, which are equipped with duplicate metering units without the installation flow means measuring the heat combustion. Emphasis is placed on the fact that a large number of measuring systems are built on the method of variable pressure drop with the use of standard orifice devices. It is pointed out that this method, according to its physical principle, measures the mass gas flow rate. It is also stipulated that ultrasonic gas meters are often used to complete duplicate metering units. The advantages of ultrasonic meters are given. Attention is drawn to the availability of technical metrological support in Ukraine on the basis calibration prover, which includes two secondary standards gas volume and volume flow rate units. Methods and technical means for determining the natural gas heat combustion are analyzed. The calculation of the gas heat combustion and the Wobbe number based on the density values is shown. It is noted that the value of the gas mass flow rate is related to the value of the gas volume flow rate precisely the value of density. The nonlinear dependence of the gas mass heat combustion for the density, which is associated with a disproportionate change in the percentage of carbon atoms to hydrogen atoms, is shown. The structural scheme of the measuring system with the duplicating metering unit for gas density definition and gas heat combustion calculation is developed. The density calculation and natural gas heat combustion depending on the molar fraction of nitrogen and carbon dioxide in the gas from the minimum to the maximum value is carried out. The linear dependence of the change in the gas heat combustion for the molar fraction of nitrogen is established, on the basis of which the method of controlling the gas heat combustion for measuring systems with a duplicate metering unit is proposed. It is shown that the developed procedure for determining the natural gas heat combustion based on the value of density, which is obtained from the calculation of gas mass flow rate and gas volume flow rate consumption on measuring systems with duplicate metering units exactly satisfies class B and C according to DSTU OIML R 140.
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Conference papers on the topic "Complete combustion"

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Laghai, A., S. H. Nabavi, H. B. Servati, and F. Syed. "IR-Laser Initiated Combustion - A Step Toward Complete Combustion." In International Congress & Exposition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 1996. http://dx.doi.org/10.4271/960464.

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Razmara, Nayyer, and Rahim Khoshbakhti Saray. "Exergy Analysis of a Simple Gas Turbine System Considering Combustion Process as Complete Combustion and Equilibrium Combustion." In ASME 2010 10th Biennial Conference on Engineering Systems Design and Analysis. ASMEDC, 2010. http://dx.doi.org/10.1115/esda2010-24997.

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Exergy analysis provides useful information for the system optimization. An exergy analysis identifies the sources of thermodynamic inefficiencies by evaluating the exergy destruction within each system component. The present work is an attempt to compare the effect of variations of species concentrations of the combustion process in a simple gas turbine system. Therefore, using a Complete combustion model and an Equilibrium combustion program model, the exergetic evaluation is carried out for a simple gas turbine system with a rated output power of 30 MW. The Complete combustion involves O2, N2, CO2, H2O and Equilibrium combustion model involves N2, O2, CO2, H2O, CO, H2, H, O, OH, N, NO as the species of combustion products. In this work, Equilibrium combustion products were calculated using Olikara and Borman method. Also, a principle of division of chemical availability (exergy) into oxidation availability, reduction availability and diffusion availability has been investigated in these models. Expression involving the variables for exergetic efficiency, exergy destruction, and chemical availability in the components of the gas turbine cycle are derived. The exergy losses and efficiencies of components based on both Complete combustion and Equilibrium combustion models are evaluated. The exergetic efficiencies of the plant based on Complete combustion and Equilibrium combustion are determined to be 28.11% and 28.16%, respectively. It is found that, variation of species has negligible effect on the system main parameters. It is also concluded that chemical exergy in Equilibrium combustion is a little more than that of Complete combustion. Because of additional species involved in Equilibrium combustion, reduction availability and oxidation availability are defined in this modeling beside diffusion availability and it increases chemical exergy of equilibrium combustion modeling. The results obtained here show that in the analysis of the power plant cycles, a simple combustion model (i.e. Complete combustion model) is in good agreement with a complex combustion model considering various species (i.e. Equilibrium combustion model). As a result, there is negligible difference between results of the mentioned combustion models and the simple Complete combustion model facilitates the analysis of such processes.
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Birkby, P., R. S. Cant, W. N. Dawes, A. A. J. Demargne, P. C. Dhanasekaran, W. P. Kellar, N. C. Rycroft, A. M. Savill, R. L. G. M. Eggels, and I. K. Jennions. "CFD Analysis of a Complete Industrial Lean Premixed Gas Turbine Combustor." In ASME Turbo Expo 2000: Power for Land, Sea, and Air. American Society of Mechanical Engineers, 2000. http://dx.doi.org/10.1115/2000-gt-0131.

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The introduction of lean premixed combustion technology in industrial gas turbines has led to a number of interesting technical issues. Lean premixed combustors are especially prone to acoustically-coupled combustion oscillations as well as to other problems of flame stability such as flashback. Clearly it is very important to understand the physics that lies behind such behaviour in order to produce robust and comprehensive remedies, and also to underpin the future development of new combustor designs. Simulation of the flow and combustion using Computational Fluid Dynamics (CFD) offers an attractive way forward, provided that the modelling of turbulence and combustion is adequate and that the technique is applicable to real industrial combustor geometries. The paper presents a series of CFD simulations of the Rolls-Royce Trent industrial combustor carried out using the McNEWT unstructured code. The entire combustion chamber geometry is represented including the premixing ducts, the fuel injectors and the discharge nozzle. A modified k-ε model has been used together with an advanced laminar flamelet combustion model that is sensitive to variations in fuel-air mixture stoichiometry. Detailed results have been obtained for the non-reacting flow field, for the mixing of fuel and air and for the combustion process itself at a number of different operating conditions. The study has provided a great deal of useful information on the operation of the combustor and has demonstrated the value of CFD-based combustion analysis in an industrial context.
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Tolstov, G. I., I. A. Medvedkov, D. P. Porfiriev, M. V. Zagidullin, A. M. Mebel, and V. N. Azyazov. "MODELING OF THE COMPLETE MECHANISM OF OXIDATION OF PHENYL RADICAL UNDER COMBUSTION CONDITIONS." In 9TH INTERNATIONAL SYMPOSIUM ON NONEQUILIBRIUM PROCESSES, PLASMA, COMBUSTION, AND ATMOSPHERIC PHENOMENA. TORUS PRESS, 2020. http://dx.doi.org/10.30826/nepcap9a-11.

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Quantum chemical calculations, computational fluid dynamics (CFD) simulations, and isothermal approximation were applied for the interpretation of experimental measurements of the reaction of С6Н5 + O2 in the high-temperature microreactor and of the pressure drop in the flow tube of the reactor.
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Catania, Andrea Emilio, Alessandro Ferrari, and Michele Manno. "Development and Application of a Complete Common-Rail Injection System Mathematical Model for Hydrodynamic Analysis and Diagnostics." In ASME 2005 Internal Combustion Engine Division Spring Technical Conference. ASMEDC, 2005. http://dx.doi.org/10.1115/ices2005-1018.

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A rather complete mathematical model for a Common Rail injection-system dynamics numerical simulation was developed to support experimentation, layout and control design, as well as performance optimization. The thermo-fluid dynamics of the hydraulic system components, including rail, connecting pipes and injectors was modeled in conjunction with the solenoid-circuit electromagnetics and the mechanics of mobile elements. Onedimensional flow equations in conservation form were used to simulate wave propagation phenomena throughout the high-pressure connecting pipes, including the feeding pipe of the injector nozzle. In order to simulate the temperature variations due to the fuel compressibility, the energy equation was used in addition to mass conservation and momentum balance equations. Besides, the possible cavitation phenomena effects on the mass flow rate through the injector bleed orifice and the nozzle holes were taken into account. A simple model of the electromagnetic driving circuit was used to predict the temporal distribution of the force acting on the pilot-valve anchor. It was based on the experimental time-histories of the current through the solenoid and of the associated voltage that is provided by the electronic control unit (ECU) to the solenoid valve. The numerical code was validated through the comparison of the prediction results with experimental data, that is, pressure, injected flow rate and needle lift time-histories, taken on a high performance test bench Moehwald-Bosch MEP2000-CA4000. The novel injection-system mathematical model was applied to the analysis of transient flows through the hydraulic circuit of a commercial multijet second-generation Common Rail system, paying specific attention to the wave propagation phenomena, to their dependence on solenoid energizing time and rail pressure, as well as to their effects on system performance. An insight was also given into the model capability of accurately predicting the wave dynamics effects on the rate and mass of fuel injected when the dwell time between two consecutive injections is varied.
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Breaux, Baine B., Srinibas Karmakar, Shengrong Zhu, and Sumanta Acharya. "Evaluation of Hydrous Ethanol Combustion in a Swirl-Stabilized Combustor." In ASME 2011 International Mechanical Engineering Congress and Exposition. ASMEDC, 2011. http://dx.doi.org/10.1115/imece2011-63688.

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The use of commercial hydrous ethanol reduces the energy cost of producing that fuel, and results in a larger net energy gain per dollar invested. Current production of commercial grade ethanol contains 5% water, and is used routinely in gasoline engines, primarily as an additive, and is currently being considered for use in gas turbines. In this study ethanol is burned in a swirl-stabilized combustor, air is introduced at a constant flow rate through a dump diffuser, and fuels ranging from 0%–20% water in ethanol are injected via pressure-orifice atomizing nozzles. The goal of the study is to examine the combustion characteristics of hydrous ethanol and to make an assessment of its suitability for a gas turbine engine. The flame structure is observed using high speed OH and CH radical chemiluminescence imaging. These observations, combined with overall metrics such as lean blowout, flame holding, heat release and emissions, are a necessity in obtaining the complete picture of hydrous ethanol combustion and are required to fully evaluate hydrous fuel as an option in continuous flame applications.
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Majidi, Kitano. "CFD Modeling of Non-Premixed Combustion in a Gas Turbine Combustor." In ASME 2002 Joint U.S.-European Fluids Engineering Division Conference. ASMEDC, 2002. http://dx.doi.org/10.1115/fedsm2002-31404.

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In the present study numerical calculations are used to solve reacting flow in a gas turbine combustor. A 3-D Favre-Averaged Navier-Stokes solver for a mixture of chemically reacting gases is applied to predict the flow pattern, gas temperature and fuel and species concentrations in the entire combustor. The complete combustor geometry with all important details such as air swirler vane passages and secondary holes are modeled. The calculations are carried out using three different turbulence models. Comparisons are made between the standard k-ε model, RNG k-ε model and a Reynolds stress transport model. To provide a closure for the chemical source term the Eddy Dissipation model is used. A lean direct injection of a liquid fuel is employed. Furthermore the influence of radiation will be investigated.
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Tauzia, Xavier, Pascal Chesse, Jean-Franc¸ois Hetet, and Arnaud Bonin. "ME´RIME´E: A Simulation Software to Study Diesel Engines Used for Military Propulsion." In ASME 2002 Internal Combustion Engine Division Fall Technical Conference. ASMEDC, 2002. http://dx.doi.org/10.1115/icef2002-494.

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The design and development of internal combustion engines, and by extension of complete powertrains for ground vehicles, constitute a particularly complex, costly and time consuming task. As a result, numerical simulation is now commonly used by engine manufacturers and vehicle designers in addition to test bench experiments. Engine simulation codes can be divided into three main categories, with very different objectives and levels of complexity: CFD codes, thermodynamic codes and real time codes. This paper presents the MERIMEE simulation code, which belongs to the second category (MERIMEE is the French acronym for Computer Research and Study Model for Engines and their Equipment). Jointly developed by Ecole Centrale de Nantes (for the models) and the CS-SI Company (for the software development) it is used by ETAS (French Army) for the development and study of complete powertrains designed for military ground propulsion. The main models used to simulate the engine behavior are first briefly described. Then, the software architecture, the interface as well as the programming and numerical aspects are described. Finally, some significant results are shown and compared with experimental data. They deal with steady state and transient engine behavior in addition to the evaluation of pollutant emissions.
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Goldstein, Harvey N., Wayne Brown, Vincent J. Tursi, and Charles W. Kenney. "Advanced Fluidized-Bed Combustor Firing Waste Coal: A Case Study." In 17th International Conference on Fluidized Bed Combustion. ASMEDC, 2003. http://dx.doi.org/10.1115/fbc2003-148.

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This paper describes the integration of an advanced fluidized-bed combustor with other technologies into a complete system that will fire waste coal blended with purchased coal to produce steam, electricity, and structural building products. The integrated system provides remediation of a waste coal pile, meets stringent environmental standards, and is economically viable.
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Medvedkov, I. A., G. I. Tolstov, D. P. Porfiriev, M. V. Zagidullin, A. M. Mebel, and V. N. Azyazov. "Simulation of the complete mechanism of oxidation of phenyl radical under combustion conditions." In INTERNATIONAL CONFERENCE ON PHYSICS AND CHEMISTRY OF COMBUSTION AND PROCESSES IN EXTREME ENVIRONMENTS (COMPHYSCHEM’20-21) and VI INTERNATIONAL SUMMER SCHOOL “MODERN QUANTUM CHEMISTRY METHODS IN APPLICATIONS”. AIP Publishing, 2020. http://dx.doi.org/10.1063/5.0034327.

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Reports on the topic "Complete combustion"

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Beaudet, R. A. Combustion-related studies using weakly-bonded complexes. Office of Scientific and Technical Information (OSTI), March 1992. http://dx.doi.org/10.2172/6856817.

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Beaudet, R. A. Combustion-related studies using weakly-bonded complexes. Office of Scientific and Technical Information (OSTI), April 1990. http://dx.doi.org/10.2172/10123737.

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Beaudet, R. A. Combustion-related studies using weakly-bonded complexes. Three year progress report. Office of Scientific and Technical Information (OSTI), March 1992. http://dx.doi.org/10.2172/10111682.

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Beaudet, R. A. Combustion-related studies using weakly-bonded complexes. Progress report, August 1, 1992--July 31, 1993. Office of Scientific and Technical Information (OSTI), June 1993. http://dx.doi.org/10.2172/10123722.

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Chan, S. H., and P. J. Janke. Complex Equilibrium Calculations of Nonideal Multiphase Systems (CEC- NMS) and Applications to Liquid Metal Fuel Combustion. Fort Belvoir, VA: Defense Technical Information Center, March 1989. http://dx.doi.org/10.21236/ada209990.

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Rappe, Andrew M. New Tools for the Study of Combustion Chemistry and Complex Gas-Surface Interactions from First Principles. Fort Belvoir, VA: Defense Technical Information Center, October 2007. http://dx.doi.org/10.21236/ada473091.

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Ekoto, Isaac, and Robert Barlow. Development of a Raman spectroscopy technique to detect alternate transportation fuel hydrocarbon intermediates in complex combustion environments. Office of Scientific and Technical Information (OSTI), December 2012. http://dx.doi.org/10.2172/1088079.

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