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Journal articles on the topic 'Solid Combustion'

Author: Grafiati

Published: 4 June 2021

Last updated: 7 February 2022

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1

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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2

Liu, Xiang Jun, and Yu Jiao Fan. "Modeling of a Ten-Particle Char Cluster Interactive Combustion." Advanced Materials Research 953-954 (June 2014): 1250–53. http://dx.doi.org/10.4028/www.scientific.net/amr.953-954.1250.

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Char-cluster interactive combustion occurs widely in practical combustors. A 3-D mathematical model for char-cluster combustion is established. The combustion and gas-solid drag properties of a ten-particle char cluster are numerically studied. Detailed results regarding velocity vector, mass component, temperature distributions around and inside the cluster are revealed. Gas-solid drag forces acted on each combusting char particle are obtained and comparatively studied.

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3

Yang, Pengnian, Zhixun Xia, Likun Ma, et al. "Direct-Connect Test of Solid Scramjet with Symmetrical Structure." Energies 14, no. 17 (2021): 5589. http://dx.doi.org/10.3390/en14175589.

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The solid scramjet has become one of the most promising engine types. In this paper, we report the first direct-connect test of a solid scramjet with symmetrical structure, carried out using boron-based fuel-rich solid propellant as fuel. During the test, which simulated a flight environment at Mach 5.6 and 25 km, the performance of the solid scramjet was obtained by measuring the pressure, thrust, and mass flow. The results show that, due to the change in the combustion area of the propellant and the deposition of the throat in the gas generator during the test, the equivalence ratio graduall

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4

Johari, Anwar, Ramli Mat, Mohd Johari Kamaruddin, Tuan Amran Tuan Abdullah, Wan Rosli Wan Sulaiman, and Asmadi Ali. "Combustion of Municipal Solid Waste in a Pilot Scale Fluidized Bed Combustor." Advanced Materials Research 931-932 (May 2014): 1015–19. http://dx.doi.org/10.4028/www.scientific.net/amr.931-932.1015.

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Combustion study of municipal solid waste combustion in a pilot scale fluidized bed combustor had been carried out. The work was aimed at demonstrating sustainable combustion of municipal solid waste by employing operating parameters gained from previous studies. The primary and secondary air factor used were AF = 0.8 and AF = 0.6 respectively. The fluidization number was 5Umf and both in-bed and freeboard region temperature distributions were monitored continuously. Results on the combustion studies revealed that the initial bed temperature could be sustained due to high thermal capacity of s

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5

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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6

Viljoen, Hendrik J., and Vladimir Hlavacek. "Deflagration and detonation in solid-solid combustion." AIChE Journal 43, no. 11 (1997): 3085–94. http://dx.doi.org/10.1002/aic.690431119.

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7

THIART, JACOB J., HENDRIK J. VILJOEN, NICOLAAS F. J. VAN RENSBURG, JORGE E. GATICA, and VLADIMIR HLAVACEK. "Stability of Non-Adiabatic Solid-Solid Combustion." Combustion Science and Technology 82, no. 1-6 (1992): 185–204. http://dx.doi.org/10.1080/00102209208951819.

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8

Miljkovic, Biljana. "Experimental facility for analysis of biomass combustion characteristics." Thermal Science 19, no. 1 (2015): 341–50. http://dx.doi.org/10.2298/tsci120928119m.

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The objective of the present article is to present an experimental facility which was designed and built at the Faculty of Technical Sciences in order to study the combustion of different sorts of biomass and municipal solid waste. Despite its apparent simplicity, direct combustion is a complex process from a technological point of view. Conventional combustion equipment is not designed for burning agricultural residues. Devices for agricultural waste combustion are still in the development phase, which means that adequate design solution is presently not available at the world market. In orde

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9

Karpenko, E. I., V. E. Messerle, and A. B. Ustimenko. "Plasma-aided solid fuel combustion." Proceedings of the Combustion Institute 31, no. 2 (2007): 3353–60. http://dx.doi.org/10.1016/j.proci.2006.07.038.

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10

Bychkov, V. V., and M. A. Liberman. "Stability of Solid Propellant Combustion." Physical Review Letters 74, no. 11 (1995): 2148. http://dx.doi.org/10.1103/physrevlett.74.2148.

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11

Lowe, C. A., and J. F. Clarke. "Aspects of solid propellant combustion." Philosophical Transactions of the Royal Society of London. Series A: Mathematical, Physical and Engineering Sciences 357, no. 1764 (1999): 3639–53. http://dx.doi.org/10.1098/rsta.1999.0514.

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12

Molchadskii, I. S., N. K. Grinevitskii, B. S. Limonov, et al. "Measuring solid mass-combustion rates." Combustion, Explosion, and Shock Waves 25, no. 2 (1989): 177–80. http://dx.doi.org/10.1007/bf00742012.

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13

Pampuch, R., J. Lis, L. Stobierski, and M. Tymkiewicz. "Solid combustion synthesis of Ti3SiC2." Journal of the European Ceramic Society 5, no. 5 (1989): 283–87. http://dx.doi.org/10.1016/0955-2219(89)90022-8.

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14

Wang, Jinsheng, and Edward J. Anthony. "Clean combustion of solid fuels." Applied Energy 85, no. 2-3 (2008): 73–79. http://dx.doi.org/10.1016/j.apenergy.2007.07.002.

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15

Bychkov, V. V., and M. A. Liberman. "Stability of Solid Propellant Combustion." Physical Review Letters 73, no. 14 (1994): 1998–2000. http://dx.doi.org/10.1103/physrevlett.73.1998.

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16

Park, C. W., and M. Kaviany. "Combustion-Thermoelectric Tube." Journal of Heat Transfer 122, no. 4 (2000): 721–29. http://dx.doi.org/10.1115/1.1318210.

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In direct combustion-thermoelectric energy conversion, direct fuel injection and reciprocation of the air flowing in a solid matrix are combined with the solid-gas interfacial heat transfer and the solid conduction to allow for obtaining superadiabatic temperatures at the hot junctions. While the solid conductivity is necessary, the relatively large thermal conductivity of the available high-temperature thermoelectric materials (e.g., Si–Ge alloys) results in a large conduction loss from the hot junctions and deteriorates the performance. Here, a combustion-thermoelectric tube is introduced an

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17

Muthuramana, Marisamy, Tomoaki Namioka, and Kunio Yoshikawa. "B208 EFFECTS OF MUNICIPAL SOLID WASTE BLENDING ON THE COAL COMBUSTION CHARACTERISTICS BY TGA ANALYSIS(Combustion-6)." Proceedings of the International Conference on Power Engineering (ICOPE) 2009.2 (2009): _2–123_—_2–127_. http://dx.doi.org/10.1299/jsmeicope.2009.2._2-123_.

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18

Gulyurtlu, I., T. Crujeira, M. H. Lopes, et al. "The Study of Combustion of Municipal Waste in a Fluidized Bed Combustor." Journal of Energy Resources Technology 128, no. 2 (2006): 123–28. http://dx.doi.org/10.1115/1.2191507.

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The combustion behavior of municipal solid waste was studied in a pilot fluidized bed combustor. The waste was pelletized prior to its use. Both co-firing with coal and combustion of waste alone were under taken. The combustion studies were carried out on the pilot installation of INETI. The fluidized bed combustor is square in cross section with each side being 300mm long. Its height is 5000mm. There is a second air supply to the freeboard at different heights to deal with high volatile fuels. There was a continuous monitoring of the temperatures in the bed, as well as the composition of the

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19

Qin, Zhao, Jiang Wu, Rui Qi Shen, Ying Hua Ye, and Li Zhi Wu. "Laser-Controlled Combustion of Solid Propellant." Advanced Materials Research 884-885 (January 2014): 87–90. http://dx.doi.org/10.4028/www.scientific.net/amr.884-885.87.

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This paper describes experimental work on laser-controlled combustion of solid propellants. Combustion of AP/HTPB, including ignition, combustion, extinction and re-ignition could be controlled by CO2 laser irradiation at the back pressure of 0.1, 0.3 and 0.5 MPa in nitrogen. Burning rate of propellant increased linearly with the increasing of laser power density. Vieilles law was used here to check pressure effect to burning rate, pressure exponent under different power density (except 0.5 MW/m2) are very close to 0.17.

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20

HOSOKAWA, Hideaki, Yukinori SAKUMA, and Satoshi OKAJIMA. "Combustion Characteristic of Solid Waste Fuels in Flowing Combustion Gas." Proceedings of Conference of Hokuriku-Shinetsu Branch 2003.40 (2003): 63–64. http://dx.doi.org/10.1299/jsmehs.2003.40.63.

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21

Saxena, S. C. "Fluidized-bed incineration of solid pellets: Combustion and co-combustion." Energy Conversion and Management 39, no. 1-2 (1998): 127–41. http://dx.doi.org/10.1016/s0196-8904(96)00116-1.

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22

Pries, Michael, Andreas Fiolitakis, and Peter Gerlinger. "Numerical Investigation of a High Momentum Jet Flame at Elevated Pressure: A Quantitative Validation with Detailed Experimental Data." Journal of the Global Power and Propulsion Society 4 (December 18, 2020): 264–73. http://dx.doi.org/10.33737/jgpps/130031.

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The development of efficient low emission combustion systems requires methods for an accurate and reliable prediction of combustion processes. Computational Fluid Dynamics (CFD) in combination with combustion modelling is an important tool to achieve this goal. For an accurate computation adequate boundary conditions are crucial. Especially data for the temperature distribution on the walls of the combustion chamber are usually not available. The present work focuses on numerical simulations of a high momentum jet flame in a single nozzle FLOX® type model combustion chamber at elevated pressur

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23

Bee´r, J. M., and R. V. Garland. "A Coal-Fueled Combustion Turbine Cogeneration System With Topping Combustion." Journal of Engineering for Gas Turbines and Power 119, no. 1 (1997): 84–92. http://dx.doi.org/10.1115/1.2815567.

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Cogeneration systems fired with coal or other solid fuels and containing conventional extracting-condensing or back pressure steam turbines can be found throughout the world. A potentially more economical plant of higher output per unit thermal energy is presented that employs a pressurized fluidized bed (PFB) and coal carbonizer. The carbonizer produces a char that is fed to the PFB and a low heating value fuel gas that is utilized in a topping combustion system. The topping combustor provides the means for achieving state-of-the-art turbine inlet temperatures and is the main contributor to e

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24

Razmyslov, A. V., and V. G. Sultanov. "Numerical modeling of gasification and combustion of solid fuels in a solid fuel ramjet combustor." Journal of Physics: Conference Series 1385 (November 2019): 012051. http://dx.doi.org/10.1088/1742-6596/1385/1/012051.

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25

Kuo, J. T., W. S. Hsu, and T. C. Yo. "Effect of Air Distribution on Solid Fuel Bed Combustion." Journal of Energy Resources Technology 119, no. 2 (1997): 120–28. http://dx.doi.org/10.1115/1.2794975.

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One important aspect of refuse mass-burn combustion control is the manipulation of combustion air. Proper air manipulation is key to the achievement of good combustion efficiency and reduction of pollutant emissions. Experiments, using a small fix-grate laboratory furnace with cylindrical combustion chamber, were performed to investigate the influence of undergrate/sidewall air distribution on the combustion of beds of wood cubes. Wood cubes were used as a convenient laboratory surrogate of solid refuse. Specifically, for different bed configurations (e.g., bed height, bed voidage, bed fuel si

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26

Boggs, Thomas L. "THE HAZARDS OF SOLID PROPELLANT COMBUSTION." International Journal of Energetic Materials and Chemical Propulsion 4, no. 1-6 (1997): 233–67. http://dx.doi.org/10.1615/intjenergeticmaterialschemprop.v4.i1-6.280.

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27

Young, Gregory, Grant A. Risha, Amber G. Miller, Russell A. Glass, Terrence L. Connell, Jr., and Richard A. Yetter. "COMBUSTION OF ALANE-BASED SOLID FUELS." International Journal of Energetic Materials and Chemical Propulsion 9, no. 3 (2010): 249–66. http://dx.doi.org/10.1615/intjenergeticmaterialschemprop.v9.i3.50.

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28

Ohlemiller, T. "Smoldering Combustion Propagation On Solid Wood." Fire Safety Science 3 (1991): 565–74. http://dx.doi.org/10.3801/iafss.fss.3-565.

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29

Toftegaard, Maja B., Jacob Brix, Peter A. Jensen, Peter Glarborg, and Anker D. Jensen. "Oxy-fuel combustion of solid fuels." Progress in Energy and Combustion Science 36, no. 5 (2010): 581–625. http://dx.doi.org/10.1016/j.pecs.2010.02.001.

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30

Adánez, J., A. Abad, T. Mendiara, P. Gayán, L. F. de Diego, and F. García-Labiano. "Chemical looping combustion of solid fuels." Progress in Energy and Combustion Science 65 (March 2018): 6–66. http://dx.doi.org/10.1016/j.pecs.2017.07.005.

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31

Whitney, S. E., and H. J. Viljoen. "Natural convection and solid phase combustion." Chemical Engineering Communications 190, no. 3 (2003): 393–430. http://dx.doi.org/10.1080/00986440302137.

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32

LEION, H., T. MATTISSON, and A. LYNGFELT. "Solid fuels in chemical-looping combustion." International Journal of Greenhouse Gas Control 2, no. 2 (2008): 180–93. http://dx.doi.org/10.1016/s1750-5836(07)00117-x.

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33

Kuz’mina, R. I., and E. I. Kovalenko. "High-efficient solid-fuel combustion catalysts." Journal of Physics: Conference Series 1347 (December 2019): 012043. http://dx.doi.org/10.1088/1742-6596/1347/1/012043.

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34

Raghunandan, B. N., E. R. Ravichandran, and A. G. Marathe. "Combustion related to solid-fuel ramjets." Journal of Propulsion and Power 1, no. 6 (1985): 502–4. http://dx.doi.org/10.2514/3.22837.

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35

M., HEGAB. "MODELING OF MICROSCALE SOLID PROPELLANT COMBUSTION." International Conference on Aerospace Sciences and Aviation Technology 10, ASAT CONFERENCE (2003): 1–24. http://dx.doi.org/10.21608/asat.2013.24421.

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36

Bebernes, J. W. "Solid duel combustion some mathematical problems." Rocky Mountain Journal of Mathematics 16, no. 3 (1986): 417–34. http://dx.doi.org/10.1216/rmj-1986-16-3-417.

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37

Asthana, S. N., R. B. Mundada, P. A. Phawade, and P. G. Shrotri. "Combustion Behaviour of Advanced Solid Propellants." Defence Science Journal 43, no. 3 (1993): 269–73. http://dx.doi.org/10.14429/dsj.43.4285.

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38

Vadchenko, S. G., I. P. Borovinskaya, and A. G. Merzhanov. "Solid-flame combustion of thin films." Doklady Physical Chemistry 408, no. 1 (2006): 123–25. http://dx.doi.org/10.1134/s0012501606050046.

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39

Rashkovsky, S. A. "Metal Agglomeration in Solid Propellants Combustion." Combustion Science and Technology 136, no. 1 (1998): 125–48. http://dx.doi.org/10.1080/00102209808924168.

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40

Rashkovsky, S. A. "Metal Agglomeration in Solid Propellants Combustion." Combustion Science and Technology 136, no. 1 (1998): 149–69. http://dx.doi.org/10.1080/00102209808924169.

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41

Brailovsky, I., and G. Sivashinsky. "Chaotic dynamics in solid fuel combustion." Physica D: Nonlinear Phenomena 65, no. 1-2 (1993): 191–98. http://dx.doi.org/10.1016/0167-2789(93)90014-r.

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42

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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43

Ciezki, Helmut K., Joachim Sender, Walter Clauß, Albert Feinauer, and Albert Thumann. "Combustion of Solid-Fuel Slabs Containing Boron Particles in Step Combustor." Journal of Propulsion and Power 19, no. 6 (2003): 1180–91. http://dx.doi.org/10.2514/2.6938.

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44

Kozin, V. S. "Effect of the thermal and gas-dynamic properties of solid rocket propellant particles on the propellant combustion rate." Technical mechanics 2021, no. 1 (2021): 63–67. http://dx.doi.org/10.15407/itm2021.01.063.

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The aim of this work is to eliminate the explosion possibility of a rocket engine that operates on a fast-burning solid propellant. The problem is considered by analogy with experiments conducted earlier. Various ways to increase the propellant combustion rate are presented. Examples of how the solid propellant combustion rate depends on the metal fuel and the oxidizer particle size are given. It is shown that unstable combustion of a solid propellant at high combustion chamber pressures is due to unstable combustion of the gas phase in the vicinity of the bifurcation point. Zeldovich’s theory

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45

Luo, Ming, Shu Zhong Wang, and Long Fei Wang. "Advances in Chemical-Looping Combustion for Solid Fuels." Applied Mechanics and Materials 316-317 (April 2013): 99–104. http://dx.doi.org/10.4028/www.scientific.net/amm.316-317.99.

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Chemical-looping combustion (CLC) is a new method for the combustion of fuels with inherent separation of carbon dioxide, which can simultaneously improve combustion efficiency and reduce environmental pollution. Since solid coal is considerably more abundant than natural gas, it would be highly advantageous if the CLC process could be adapted for solid fuels. The present review introduces the technical approaches for the solid fuels CLC process, and the existing technical problems in solid fuels CLC are discussed. The demands in oxygen carriers of chemical looping combustion for solid fuels a

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46

Trnka, Juraj, Jozef Jandačka, and Michal Holubčík. "Influence of Biomass Combustion Method on Properties of Solid Fuel Residues." MATEC Web of Conferences 328 (2020): 04001. http://dx.doi.org/10.1051/matecconf/202032804001.

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The correct course of the combustion process has a great influence on several output parameters. In addition to the impact on the performance and efficiency of the device, the impact on the formation and properties of gaseous emissions and solid residue is particularly noticeable. The solid combustion residue, in particular in the form of ash, remains trapped as the final product after combustion in the incinerator or may be released to the outside environment. Improperly, combustion can form two negative extremes. The first extreme is the formation of too fine dust particles of ash and solid

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47

Wang, Wei, Jiang Li, Ke Zhang, and Yang Liu. "Computing Method Investigation and Verification of Gas-Solid Combustion in Magnesium-Aluminum Based Propellant Ducted Rocket." Advanced Materials Research 503-504 (April 2012): 490–93. http://dx.doi.org/10.4028/www.scientific.net/amr.503-504.490.

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The combustion mechanism, which consisting of 22 species and 23 reaction equations, and three discrete models such as inertia, combusting, modification droplet, are employed for the investigation of gas-solid combustion in magnesium-aluminum based propellant ducted rocket based on thermal performance calculation. And path lines, temperature distribution, sediments are discussed after the computing method is validated by direct-connect experimentation and the flow field information, which obtained by numerical method and coincided with currently conclusions. The results indicated that the propo

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48

Samuelsen, Scott, and Amy Babcock. "Coal Without Combustion." Mechanical Engineering 129, no. 04 (2007): 30–33. http://dx.doi.org/10.1115/1.2007-apr-2.

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This article focuses on various researches that have been undertaken to study and test use of fuel cells instead of boilers for cheap and clean electricity production. One of the most ambitious projects is the Solid State Energy Conversion Alliance (SECA), created by the U.S. Department of Energy to clear the technical hurdles that have kept fuel cells impractical. Compared to other government research programs, SECA has an unusual structure. The program unifies several organizations to work toward a common goal, yet retains a healthy spirit of competition to drive progress and spur innovation

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49

Chen, X. Y., Yong Feng Zhang, Q. C. Zhang, and Q. Zhou. "Oxygen-Enriched Combustion Characteristics of Solid Fuel - The Lignite." Key Engineering Materials 693 (May 2016): 594–96. http://dx.doi.org/10.4028/www.scientific.net/kem.693.594.

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Oxygen-enriched Combustion behavior of indigenous lignite was investigated by using thermo gravimetric analyzer (TG). Combustion tests were carried out in six different atmospheres. The experiment results showed the oxygen–enriched atmosphere can improve the combustion rate of the lignite and expand the application scope of the lignite. Determine the Combustibility index to reveal the oxygen-enriched combustion process in detail.

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50

Kraszkiewicz, Artur, Francesco Santoro, and Simone Pascuzzi. "Emmission of Sulphur Oxides from Agricultural Solid Biofuels Combustion." Agricultural Engineering 24, no. 4 (2020): 35–45. http://dx.doi.org/10.1515/agriceng-2020-0034.

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Abstract In the aspect of the course and analysis of products of biomass fuels combustion in grill feed boilers, the combustion process of wheat straw and meadow hay were assessed taking into consideration conditions of SO2 emission. Different types of briquettes used in the research not only had various chemical properties but also physical properties. In the aspect of assessment of energy and organic parameters of the combustion process, the sulphur content in biomass becomes a significant factor at its energy use. Registered emission during combustion of meadow hay biomass referred to wheat

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