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Letteratura scientifica selezionata sul tema "Combustion"

Autore: Grafiati

Pubblicato: 4 giugno 2021

Ultima modifica: 25 luglio 2025

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Articoli di riviste sul tema "Combustion"

1

Ran, Jing Yu, Li Juan Liu, Chai Zuo Li, and Li Zhang. "Numerical Study on Optimum Designing of the Air Distribution Structure of a New Cyclone Combustor." Advanced Materials Research 347-353 (October 2011): 3005–14. http://dx.doi.org/10.4028/www.scientific.net/amr.347-353.3005.

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A new type of cyclone combustor is designed based on the traditional pulverized coal liquid slag combustor in this paper. According to the characteristics of swirl combustion and flow, numerical simulation of pulverized coal combustion in a new cyclone combustor has carried out using Realizable k-ε equation model with swirl modified to gas phase and stochastic trajectory model under Lagrange coordinate system to particle phase. Flows and combustion characteristics under different working conditions are mainly studied by changing the angles of primary and secondary air inlets, and then structur

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2

Li, Shou-Zhe, Yu-Long Niu, Shu-Li Cao, Jiao Zhang, Jialiang Zhang, and Xuechen Li. "The effect of plasma discharge on methane diffusion combustion in air assisted by an atmospheric pressure microwave plasma torch." Journal of Physics D: Applied Physics 55, no. 23 (2022): 235203. http://dx.doi.org/10.1088/1361-6463/ac50cb.

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Abstract An atmospheric pressure air microwave plasma torch is employed to assist methane diffusion combustions using a combination of a combustor and burner. Experimentally, the effect of the air microwave plasma on combustion is investigated with respect to the flame morphology and the variation of gas components in the exhaust with the fuel equivalence ratio φ or the methane flow rate by comparing plasma-assisted combustion (PAC) and natural combustion (NC) without plasma application. The combustion degree of CH4 in PACs is found to be much enhanced in rich fuel combustion than in NC in bot

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3

Yang, Xiaojian, and Guoming G. Zhu. "A control-oriented hybrid combustion model of a homogeneous charge compression ignition capable spark ignition engine." Proceedings of the Institution of Mechanical Engineers, Part D: Journal of Automobile Engineering 226, no. 10 (2012): 1380–95. http://dx.doi.org/10.1177/0954407012443334.

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To implement the homogeneous charge compression ignition combustion mode in a spark ignition engine, it is necessary to have smooth mode transition between the spark ignition and homogeneous charge compression ignition combustions. The spark ignition–homogeneous charge compression ignition hybrid combustion mode modeled in this paper describes the combustion mode that starts with the spark ignition combustion and ends with the homogeneous charge compression ignition combustion. The main motivation of studying the hybrid combustion mode is that the percentage of the homogeneous charge compressi

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4

Ozawa, Y., J. Hirano, M. Sato, M. Saiga, and S. Watanabe. "Test Results of Low NOx Catalytic Combustors for Gas Turbines." Journal of Engineering for Gas Turbines and Power 116, no. 3 (1994): 511–16. http://dx.doi.org/10.1115/1.2906849.

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Catalytic combustion is an ultralow NOx combustion method, so it is expected that this method will be applied to a gas turbine combustor. However, it is difficult to develop a catalytic combustor because catalytic reliability at high temperature is still insufficient. To overcome this difficulty, we designed a catalytic combustor in which premixed combustion was combined. By this device, it is possible to obtain combustion gas at a combustion temperature of 1300°C while keeping the catalytic temperature below 1000°C. After performing preliminary tests using LPG, we designed two types of combus

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5

Li, Chaolong, Zhixun Xia, Likun Ma, Xiang Zhao, and Binbin Chen. "Numerical Study on the Solid Fuel Rocket Scramjet Combustor with Cavity." Energies 12, no. 7 (2019): 1235. http://dx.doi.org/10.3390/en12071235.

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Scramjet based on solid propellant is a good supplement for the power device of future hypersonic vehicles. A new scramjet combustor configuration using solid fuel, namely, the solid fuel rocket scramjet (SFRSCRJ) combustor is proposed. The numerical study was conducted to simulate a flight environment of Mach 6 at a 25 km altitude. Three-dimensional Reynolds-averaged Navier–Stokes equations coupled with shear stress transport (SST) k − ω turbulence model are used to analyze the effects of the cavity and its position on the combustor. The feasibility of the SFRSCRJ combustor with cavity is dem

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6

Kinoshita, Y., J. Kitajima, Y. Seki, and A. Tatara. "Experimental Studies on Methane-Fuel Laboratory Scale Ram Combustor." Journal of Engineering for Gas Turbines and Power 117, no. 3 (1995): 394–400. http://dx.doi.org/10.1115/1.2814108.

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The laboratory scale ram combustor test program has been investigating fundamental combustion characteristics of a ram combustor, which operates from Mach 2.5 to 5 for the super/hypersonic transport propulsion system. In our previous study, combustion efficiency had been found poor, less than 70 percent, due to a low inlet air temperature and a high velocity at Mach 3 condition. To improve the low combustion efficiency, a fuel zoning combustion concept was investigated by using a subscale combustor model first. Combustion efficiency more than 90 percent was achieved and the concept was found v

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7

Chein, Reiyu, Yen-Cho Chen, Jui-Yu Chen, and J. N. Chung. "Premixed Methanol–Air Combustion Characteristics in a Mini-scale Catalytic Combustor." International Journal of Chemical Reactor Engineering 14, no. 1 (2016): 383–93. http://dx.doi.org/10.1515/ijcre-2014-0061.

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AbstractMethanol catalytic combustion in a mini-scale tubular quartz-made combustor is investigated in this study. An alumina sphere was employed as the support for the platinum catalyst. The experimental results showed that the combustion can be self-ignited at room temperature. Using the combustor wall temperature to characterize the combustor performance, it was found that the combustion temperature can reach a high value within a short time. The experimental results indicated that the combustor performance depends greatly on the fuel/air supply. A higher temperature can be obtained with a

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8

Ding, Shibin, Qingzhi Wang, and Weizhuo Hua. "Study on Plasma Combustion in Aeroengine Combustor." Journal of Physics: Conference Series 2483, no. 1 (2023): 012054. http://dx.doi.org/10.1088/1742-6596/2483/1/012054.

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Abstract To explore the plasma combustion affect the performance of the aircraft engine combustor, 16 components in the aviation kerosene 25-step reaction mechanism on the basis of considering step 9 simplify the plasma reaction mechanism, set up considering plasma electron collision reaction excited state relaxation and excited states participate in the process of chemical reaction kerosene combustion reaction model, The numerical calculation of the combustion process in the combustor is carried out, and the numerical calculation results of the combustion process with or without plasma combus

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9

Sing Mei, Sim, Aslina Anjang Ab Rahman, Mohd Shukur Zainol Abidin, and Nurul Musfirah Mazlan. "d2 Law and Penetration Length of Jatropha and Camelina Bio-Synthetic Paraffinic Kerosene Spray Characteristics at Take-Off, Top of Climb and Cruise." Aerospace 8, no. 9 (2021): 249. http://dx.doi.org/10.3390/aerospace8090249.

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A comparison of d2 law and penetration length of biofuels with Jet–A through the incorporation of fuel properties and actual combustor inlet data at various flight trajectories is presented. This study aims to identify fuel properties and flight operating conditions that most influence droplet characteristics accurately. The study comprises two phases involving a simulation using GSP to predict combustor inlet data for the respective flight operating conditions and a simulation using ANSYS Fluent V18.1 to obtain combustion characteristics of biofuels and Jet–A. The biofuels chosen in this stud

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10

Erdiwansyah, Mahidin, Husni Husin, et al. "Combustion Efficiency in a Fluidized-Bed Combustor with a Modified Perforated Plate for Air Distribution." Processes 9, no. 9 (2021): 1489. http://dx.doi.org/10.3390/pr9091489.

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Combustion efficiency is one of the most important parameters especially in the fluidized-bed combustor. Investigations into the efficiency of combustion in fluidized-bed combustor fuels using solid biomass waste fuels in recent years are increasingly in demand by researchers around the world. Specifically, this study aims to calculate the combustion efficiency in the fluidized-bed combustor. Combustion efficiency is calculated based on combustion results from the modification of hollow plates in the fluidized-bed combustor. The modified hollow plate aims to control combustion so that the fuel

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Più fonti

Tesi sul tema "Combustion"

1

Tajiri, Kazuya. "Simulations of combustion dynamics in pulse combustor." Thesis, Georgia Institute of Technology, 2001. http://hdl.handle.net/1853/12175.

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2

Fernandes, Renato. "Metodologia de projeto de queimadores a jato para fornos de clínquer." [s.n.], 2011. http://repositorio.unicamp.br/jspui/handle/REPOSIP/264846.

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Orientador: Waldir Antônio Bizzo<br>Dissertação (mestrado) - Universidade Estadual de Campinas, Faculdade de Engenharia Mecânica<br>Made available in DSpace on 2018-08-18T17:06:17Z (GMT). No. of bitstreams: 1 Fernandes_Renato_M.pdf: 7631607 bytes, checksum: 14334de2da1bd698c87a4fd0efbed3f4 (MD5) Previous issue date: 2011<br>Resumo: Os queimadores a jato são caracterizados pela elevada quantidade de movimento na direção axial e elevada potência, estes queimadores são muito empregados em fornos rotativos, principalmente na indústria do cimento e da calcinação. O projeto de queimadores a jato é

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3

Leng, Jing. "Combustion processes within a gas fired pulsed combustor." Thesis, University of Cambridge, 1995. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.307945.

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4

Bishop, Robert Phelps. "Combustion efficiency in internal combustion engines." Thesis, Massachusetts Institute of Technology, 1985. http://hdl.handle.net/1721.1/15164.

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Thesis (B.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1985.<br>MICROFICHE COPY AVAILABLE IN ARCHIVES AND ENGINEERING<br>Bibliography: leaf 26.<br>by Robert Phelps Bishop.<br>B.S.

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5

Hossain, Abu Norman. "Combustion of solid fuel in a fluidized bed combustor." Ohio : Ohio University, 1998. http://www.ohiolink.edu/etd/view.cgi?ohiou1176492911.

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Hossain, Abu Noman. "Combustion of solid fuel in a fluidized bed combustor." Ohio University / OhioLINK, 1998. http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1176492911.

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7

Lei, Yafeng. "Combustion and direct energy conversion in a micro-combustor." Texas A&M University, 2005. http://hdl.handle.net/1969.1/4311.

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The push toward the miniaturization of electromechanical devices and the resulting need for micro-power generation (milliwatts to watts) with low-weight, long-life devices has led to the recent development of the field of micro-scale combustion. Since batteries have low specific energy (~200 kJ/kg) and liquid hydrocarbon fuels have a very high specific energy (~50000 kJ/kg), a miniaturized power-generating device, even with a relatively inefficient conversion of hydrocarbon fuels to power, would result in increased lifetime and/or reduced weight of an electronic or mechanical system that curre

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8

Chow, Siu-Kei. "Flow and combustion characteristics of a liquid-fuelled combustor." Thesis, Imperial College London, 1991. http://hdl.handle.net/10044/1/46714.

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Ichihashi, Fumitaka. "Investigation of Combustion Instability in a Single Annular Combustor." University of Cincinnati / OhioLINK, 2011. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1299617901.

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10

Ribeiro, Natália da Silva [UNESP]. "Estudo termogravimétrico da combustão e oxicombustão de misturas carvão mineral-biomassa." Universidade Estadual Paulista (UNESP), 2017. http://hdl.handle.net/11449/149903.

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Submitted by NATALIA DA SILVA RIBEIRO null (nsribeiro2@gmail.com) on 2017-03-21T14:14:32Z No. of bitstreams: 1 Defesa Natalia_Final..pdf: 3776400 bytes, checksum: 4147b87ccc01a8c95a9e60c44f70613b (MD5)<br>Rejected by Luiz Galeffi (luizgaleffi@gmail.com), reason: Solicitamos que realize uma nova submissão seguindo a orientação abaixo: O arquivo submetido está sem a ficha catalográfica. A versão submetida por você é considerada a versão final da dissertação/tese, portanto não poderá ocorrer qualquer alteração em seu conteúdo após a aprovação. Corrija esta informação e realize uma nova

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Più fonti

Libri sul tema "Combustion"

1

Warnatz, Jürgen, Ulrich Maas, and Robert W. Dibble. Combustion. Springer Berlin Heidelberg, 1999. http://dx.doi.org/10.1007/978-3-642-98027-5.

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Warnatz, Jürgen, Ulrich Maas, and Robert W. Dibble. Combustion. Springer Berlin Heidelberg, 2001. http://dx.doi.org/10.1007/978-3-662-04508-4.

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3

Warnatz, Jürgen, Ulrich Maas, and Robert W. Dibble. Combustion. Springer Berlin Heidelberg, 1996. http://dx.doi.org/10.1007/978-3-642-97668-1.

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4

Glassman, Irvin. Combustion. 2nd ed. Academic Press, 1987.

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5

1952-, Yetter Richard A., ed. Combustion. 4th ed. Academic Press, 2008.

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6

Cottilard, Sophie A. Catalytic combustion. Nova Science Publishers, 2011.

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7

Raghavan, Vasudevan. Combustion Technology. Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-030-74621-6.

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8

Liberman, Michael A. Combustion Physics. Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-85139-2.

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Raghavan, Vasudevan. Combustion Technology. John Wiley &;#38; Sons, Ltd, 2016. http://dx.doi.org/10.1002/9781119241775.

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10

Gupta, Aman, Shubham Sharma, and Sunny Narayan. Combustion Engines. John Wiley & Sons, Inc., 2016. http://dx.doi.org/10.1002/9781119284543.

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Capitoli di libri sul tema "Combustion"

1

Zohuri, Bahman, and Patrick McDaniel. "Combustion." In Thermodynamics In Nuclear Power Plant Systems. Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-13419-2_11.

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2

Struchtrup, Henning. "Combustion." In Thermodynamics and Energy Conversion. Springer Berlin Heidelberg, 2014. http://dx.doi.org/10.1007/978-3-662-43715-5_25.

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3

Simonson, John. "Combustion." In Thermodynamics. Macmillan Education UK, 1993. http://dx.doi.org/10.1007/978-1-349-12466-4_9.

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4

Basu, Prabir. "Combustion." In Circulating Fluidized Bed Boilers. Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-06173-3_4.

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5

Sherwin, Keith, and Michael Horsley. "Combustion." In Thermofluids. Springer US, 1996. http://dx.doi.org/10.1007/978-1-4899-4433-7_21.

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Zohuri, Bahman, and Patrick McDaniel. "Combustion." In Thermodynamics in Nuclear Power Plant Systems. Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-93919-3_11.

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7

Heckel, Pamela E. "Combustion." In SpringerBriefs in Environmental Science. Springer Netherlands, 2015. http://dx.doi.org/10.1007/978-94-017-9701-6_2.

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Sherwin, Keith, and Michael Horsley. "Combustion." In Thermofluids. Springer US, 1996. http://dx.doi.org/10.1007/978-1-4899-6870-8_21.

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9

Sherwin, Keith. "Combustion." In Introduction to Thermodynamics. Springer Netherlands, 1993. http://dx.doi.org/10.1007/978-94-011-1514-8_11.

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10

Cleaves, Henderson James. "Combustion." In Encyclopedia of Astrobiology. Springer Berlin Heidelberg, 2015. http://dx.doi.org/10.1007/978-3-662-44185-5_322.

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Atti di convegni sul tema "Combustion"

1

Zagury, Pedro Athias. "QUEIMADOR DOC - DILUTE OXYGEN COMBUSTION – COMBUSTÃO DE OXIGÊNIO DILUÍDO." In 28º Seminário de Balanços Energéticos Globais e Utilidades e 22º Encontro de Produtores e Consumidores de Gases Industrais. Editora Blucher, 2007. https://doi.org/10.5151/2594-3626-2004-15502-0024.

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2

Culick, F. "Combustion instabilities - Mating dance of chemical, combustion, and combustor dynamics." In 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-3178.

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3

Inamura, Takao, Mikihiro Sei, Mamoru Takahashi, and Akinaga Kumakawa. "Combustion characteristics of ramjet combustor." In 32nd Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 1996. http://dx.doi.org/10.2514/6.1996-2665.

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4

Scarinci, Thomas, and John L. Halpin. "Industrial Trent Combustor — Combustion Noise Characteristics." In ASME 1999 International Gas Turbine and Aeroengine Congress and Exhibition. American Society of Mechanical Engineers, 1999. http://dx.doi.org/10.1115/99-gt-009.

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Thermoacoustic resonance is a difficult technical problem that is experienced by almost all lean-premixed combustors. The Industrial Trent combustor is a novel dry-low-emissions (DLE) combustor design, which incorporates three stages of lean premixed fuel injection in series. The three stages in series allow independent control of two stages — the third stage receives the balance of fuel to maintain the desired power level — at all power conditions. Thus, primary zone and secondary zone temperatures can be independently controlled. This paper examines how the flexibility offered by a 3-stage l

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Nakae, Tomoyoshi. "Combustion Control for Low NOx Combustor." In 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. American Institute of Aeronautics and Astronautics, 2002. http://dx.doi.org/10.2514/6.2002-3726.

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6

Lemcherfi, Aaron I., Rohan Gejji, Tristan L. Fuller, William E. Anderson, and Carson D. Slabaugh. "Investigation of Combustion Instabilities in a Full Flow Staged Combustion Model Rocket Combustor." In AIAA Propulsion and Energy 2019 Forum. American Institute of Aeronautics and Astronautics, 2019. http://dx.doi.org/10.2514/6.2019-3948.

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7

Barhaghi, Darioush G., and Daniel Lörstad. "Investigation of Combustion in a Dump Combustor Using Different Combustion and Turbulence Models." In ASME Turbo Expo 2015: Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2015. http://dx.doi.org/10.1115/gt2015-44095.

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Modelling combustion in gas turbine combustors remains to be a challenge since several different physical phenomena interact in the process. One of the most important aspects of the combustion in a gas turbine combustor is the chemistry-turbulence interaction. In order to study the effect of the combustion and turbulence models, a dump combustor geometry is selected. Two combustion models namely, finite rate chemistry and flamelet based models, together with different turbulent models including LES 1eq k-model, RANS k-epsilon and k-omega models are implemented using both CFX and OpenFoam codes

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8

Ge*, Bing, Yuze Li, Yuliang Jia, Min Jin, and Shusheng Zang. "Study on Combustion instability of Secondary Combustion in an Axial Staged Model Combustor." In GPPS Hong Kong24. GPPS, 2023. http://dx.doi.org/10.33737/gpps23-tc-269.

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The experimental study is carried out to reveal the influence of the disturbance of main combustion air inlet on the axial staged combustion. The response of the combustion characteristics in the primary and secondary combustion chambers are obtained by acoustically forcing the inlet air to oscillate. The results indicate that the dominant frequency of combustion oscillation in the axial staged combustor is basically as the same as that of acoustic excitation. The pressure is more pronounced at the forced frequency of 270 Hz. Compared with the stable combustion state, the reburning flame is li

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Singh, Kapil, Bala Varatharajan, Ertan Yilmaz, Fei Han, and Kwanwoo Kim. "Effect of Hydrogen Combustion on the Combustion Dynamics of a Natural Gas Combustor." In ASME Turbo Expo 2008: Power for Land, Sea, and Air. ASMEDC, 2008. http://dx.doi.org/10.1115/gt2008-51343.

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In a carbon-constrained world, Integrated Gasification Combined Cycle (IGCC) systems achieve excellent environmental performance and offer a more economical pre-combustion CO2 removal compared to other coal-based systems. The residual gas after carbon removal is comprised primarily of hydrogen and nitrogen mixtures. Achieving stable combustion of hydrogen-rich fuel mixtures while producing ultra-low NOx emissions (much lower than current diffusion combustion technology) is challenging. The goal of this study was to characterize the stability of lean premixed combustion systems operating with h

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TAMURA, HIROSHI, FUMIEI ONO, AKINAGA KUMAKAWA, and NOBUYUKI YATSUYANAGI. "LOX/methane staged combustion rocket combustor investigation." In 23rd Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 1987. http://dx.doi.org/10.2514/6.1987-1856.

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Rapporti di organizzazioni sul tema "Combustion"

1

Banerjee, Subhodeep, and Robin Hughes. Biomass Combustion in a Circulating Fluidized Bed Combustor. Office of Scientific and Technical Information (OSTI), 2020. http://dx.doi.org/10.2172/1659115.

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Hughes, Robin, and Subhodeep Banerjee. Biomass Combustion in a Circulating Fluidized Bed Combustor. Office of Scientific and Technical Information (OSTI), 2020. http://dx.doi.org/10.2172/1660765.

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3

Parr, T., K. Wilson, K. Schadow, J. Cole, and N. Widmer. Sludge Combustor Using Swirl and Active Combustion Control. Defense Technical Information Center, 2000. http://dx.doi.org/10.21236/ada382663.

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4

Beshouri. PR-309-04200-R01 Modeling Methodology for Parametric Emissions Monitoring System for Combustion Turbines. Pipeline Research Council International, Inc. (PRCI), 2005. http://dx.doi.org/10.55274/r0010731.

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Prior attempts to develop a generic Parametric Emissions Monitoring methodology for combustion turbines, particularly low emissions units, have failed due either to the reduction of a complex problem to too few degrees of freedom or the brute force reliance on regression analysis. Field test data collected by the research team clearly illustrated that a successful PEMS model will need to incorporate multiple zones to account for pilot fuel versus pre-mixed combustion, and changes in air/fuel ratio at the flame front. The information reported herein shows that, ideally, the PEMS model should re

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Gutmark, Ephralm J., and Guoqiang Li. Combustion Control in Industrial Multi-Swirl Stabilized Spray Combustor. Defense Technical Information Center, 2005. http://dx.doi.org/10.21236/ada441269.

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6

A. Levasseur, S. Goodstine, J. Ruby, et al. Combustion 2000. United Technologies Corp, 2001. http://dx.doi.org/10.2172/898342.

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Skone, Timothy J. Distribution combustion. Office of Scientific and Technical Information (OSTI), 2018. http://dx.doi.org/10.2172/1559440.

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Skone, Timothy J. Processing combustion. Office of Scientific and Technical Information (OSTI), 2018. http://dx.doi.org/10.2172/1559827.

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Ohlemiller, T. J. Smoldering combustion. National Bureau of Standards, 1986. http://dx.doi.org/10.6028/nbs.ir.85-3294.

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Ojeda, William de. Low Temperature Combustion Demonstrator for High Efficiency Clean Combustion. Office of Scientific and Technical Information (OSTI), 2010. http://dx.doi.org/10.2172/1043162.

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