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Relevant bibliographies by topics / Solid Combustion

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Academic literature on the topic 'Solid Combustion'

Author: Grafiati

Published: 4 June 2021

Last updated: 7 February 2022

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Journal articles on the topic "Solid Combustion"

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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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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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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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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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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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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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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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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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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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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Dissertations / Theses on the topic "Solid Combustion"

1

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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Lin, Dah-Chan. "Computational modelling of solid fuel combustion." Thesis, Cranfield University, 1991. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.305380.

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Butler, Albert George. "Holographic investigation of solid propellant combustion." Thesis, Monterey, California. Naval Postgraduate School, 1988. http://hdl.handle.net/10945/23252.

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Approved for public release; distribution is unlimited<br>An investigation into the behavior of aluminized solid propellant combustion in a two-dimensional windowed rocket motor was conducted using holographic techniques. Holograms were recorded in the motor port, aft of the propellant grain and at the entrance to the exhaust nozzle for two different propellant compositions at varying operating pressures. Quantitative particle size data for particles larger than 20 microns were obtained from the holograms. From these data, the mean diameters (D32) of the larger particles were calculat

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Brown, Tamaryn Ann. "Chemical-looping combustion with solid fuels." Thesis, University of Cambridge, 2011. https://www.repository.cam.ac.uk/handle/1810/252227.

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This dissertation investigates a version of CLC for solid fuels, based on a single fluidised bed reactor, operated cyclically, with each cycle containing three stages. (i) Fuel is fed steadily to a bed of oxygen-carrier fluidised with steam or CO<sub>2</sub>. The fuel is gasified and the resulting syngas is oxidised by the oxygen-carrier, which is itself reduced: unreacted char accumulates. (ii) Before the oxygen-carrier is completely converted, feeding of fuel is stopped and the remaining char in the bed is gasified. (iii) The fluidising gas is changed to air and the carrier is regenerated. E

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Radhakrishnan, Arun. "Self-sustained combustion of low grade solid fuels in a stagnation-point reverse-flow combustor." Diss., Georgia Institute of Technology, 2013. http://hdl.handle.net/1853/50275.

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This thesis investigates the use of the Stagnation-Point Reverse-Flow (SPRF) combustor geometry for burning low-grade solid fuels that are attractive for specific industrial applications because of their low cost and on-site availability. These fuels are in general, hard to burn, either because of high moisture and impurity-content, e.g. biomass, or their low-volatiles content, e.g., petroleum-coke. This results in various challenges to the combustor designer, for example reduced flame stability and poor combustion efficiency. Conventional solutions include preheating the incoming flow as well

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Cekic, Ayca. "Experimental Study Of Solid Propellant Combustion Instability." Master's thesis, METU, 2005. http://etd.lib.metu.edu.tr/upload/2/12606947/index.pdf.

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In this study, experimental investigation of solid propellant combustion instability using an end burning T-Burner setup is performed. For this purpose, a T-Burner setup is designed, analyzed, constructed and tested with all its sub components. T-Burner setup constructed is mainly composed of a base part, a control panel and the T-Burner itself. Combustion chamber, pressure stabilization mechanism, pressurization system, measurement instruments and data acquisition systems form the T-Burner. Pressure stabilization mechanism is utilized in two different alternatives, first of which is by the us

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Sørum, Lars. "Environmental aspects of municipal solid waste combustion." Doctoral thesis, Norwegian University of Science and Technology, Norwegian University of Science and Technology, 2000. http://urn.kb.se/resolve?urn=urn:nbn:no:ntnu:diva-1488.

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Kan, Tie. "Combustion of solid waste in a pulse incinerator." Diss., Georgia Institute of Technology, 1999. http://hdl.handle.net/1853/12975.

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Ou, Jenq-Jang. "The combustion of fossil and waste solid fuels." Thesis, Imperial College London, 1994. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.308074.

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Books on the topic "Solid Combustion"

1

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Combustion of solid propellants. AGARD, 1991.

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North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Combustion of solid propellants. AGARD, 1991.

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K, Kuo Kenneth, and Pein Roland, eds. Combustion of Boron-based solid propellants and solid fuels. Begell House/CRC Press, 1992.

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4

Butler, Albert George. Holographic investigation of solid propellant combustion. Naval Postgraduate School, 1988.

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5

Bernhard, Peters. Thermal conversion of solid fuels. WIT, 2003.

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6

Tillman, David A. The combustion of solid fuels and wastes. Academic Press, 1991.

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Greatrix, D. R. A model for normal acceleration effects on composite propellant combustion. [s.n.], 1989.

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8

Wall, T., L. Baxter, and R. Gupta. Impact of mineral impurities in solid fuel combustion. Kluwer Academic, 2002.

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Gupta, R. P., T. F. Wall, and L. Baxter, eds. Impact of Mineral Impurities in Solid Fuel Combustion. Kluwer Academic Publishers, 2002. http://dx.doi.org/10.1007/b118076.

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Jones, Jenny M., Amanda R. Lea-Langton, Lin Ma, Mohamed Pourkashanian, and Alan Williams. Pollutants Generated by the Combustion of Solid Biomass Fuels. Springer London, 2014. http://dx.doi.org/10.1007/978-1-4471-6437-1.

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Book chapters on the topic "Solid Combustion"

1

Raghavan, Vasudevan. "Solid Fuel Systems." In Combustion Technology. Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-74621-6_6.

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Warnatz, Jürgen, Ulrich Maas, and Robert W. Dibble. "Combustion of Liquid and Solid Fuels." In Combustion. Springer Berlin Heidelberg, 1999. http://dx.doi.org/10.1007/978-3-642-98027-5_15.

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Warnatz, Jürgen, Ulrich Maas, and Robert W. Dibble. "Combustion of Liquid and Solid Fuels." In Combustion. Springer Berlin Heidelberg, 1996. http://dx.doi.org/10.1007/978-3-642-97668-1_15.

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Warnatz, Jürgen, Ulrich Maas, and Robert W. Dibble. "Combustion of Liquid and Solid Fuels." In Combustion. Springer Berlin Heidelberg, 2001. http://dx.doi.org/10.1007/978-3-662-04508-4_15.

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Svoboda, K., M. Hartman, and J. Cermák. "Combustion Mechanisms — Solid Phase." In Pollutants from Combustion. Springer Netherlands, 2000. http://dx.doi.org/10.1007/978-94-011-4249-6_3.

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Rechberger, Helmut. "Incineration: Co-Combustion." In Solid Waste Technology & Management. John Wiley & Sons, Ltd, 2010. http://dx.doi.org/10.1002/9780470666883.ch31.

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Hanby, Victor Ian. "Solid Fuels." In Combustion and Pollution Control in Heating Systems. Springer London, 1994. http://dx.doi.org/10.1007/978-1-4471-2071-1_9.

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Cheng, S. I. "L*-Combustion Instability in Solid Propellant Rocket Combustion." In Recent Advances in the Aerospace Sciences. Springer US, 1985. http://dx.doi.org/10.1007/978-1-4684-4298-4_13.

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Jones, Jenny M., Amanda R. Lea-Langton, Lin Ma, Mohamed Pourkashanian, and Alan Williams. "The Combustion of Solid Biomass." In Pollutants Generated by the Combustion of Solid Biomass Fuels. Springer London, 2014. http://dx.doi.org/10.1007/978-1-4471-6437-1_3.

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

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Conference papers on the topic "Solid Combustion"

1

Widener, J., and M. Beckstead. "Aluminum combustion modeling in solid propellant combustion products." In 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 1998. http://dx.doi.org/10.2514/6.1998-3824.

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PARK, O., and T. CHUNG. "Combustion dynamics for solid propellants." In 26th Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-542.

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Price, E., R. Jeenu, S. Chakravarthy, and J. Seitzman. "Solid propellant combustion - Surface disproportionation." In 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-3327.

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Li, Songgeng, Weigang Lin, and Jianzhong Yao. "Radial Hydrodynamics of High Velocity Gas-Solid Down-Flow Fluidized Beds." In 17th International Conference on Fluidized Bed Combustion. ASMEDC, 2003. http://dx.doi.org/10.1115/fbc2003-123.

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Experiments have been carried out in a gas-solids co-current down-flow circulating fluidized beds. The radial profiles of particle velocity and solid concentrations were measured by a fiber optical probe. Local solid flux was calculated based on the measured local particle velocity and solid concentration. The influence of gas velocity and solid recirculation rate on the radial flow structure has been examined. The experimental results show that the radial flow structure at high gas velocity has its own prominent characteristics in comparison with that at low gas velocity.

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Jung, Woosuk, Seungkwan Baek, Taesoo Kwon, Juhyeon Park, and Sejin Kwon. "Combustion Test of Solid Fuel Ramjet Combustor Using Gas Generator." In 53rd AIAA/SAE/ASEE Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 2017. http://dx.doi.org/10.2514/6.2017-4945.

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Ecker, Tobias, Sebastian Karl, and Klaus Hannemann. "Modeling of Aluminum Particle Combustion in Solid Rocket Combustion Chambers." In 53rd AIAA/SAE/ASEE Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 2017. http://dx.doi.org/10.2514/6.2017-4781.

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Kakami, Akira, Tsutomu Takai, and Takeshi Tachibana. "Solid Propellant Combustion Under Laser Heating." In 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. American Institute of Aeronautics and Astronautics, 2008. http://dx.doi.org/10.2514/6.2008-4788.

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NAKAGAWA, I., and T. KUWAHARA. "Combustion of solid fueled ramjet. I." In 28th Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-3727.

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IIDA, A., and I. KOMAI. "Combustion of solid fueled ramjet. II." In 28th Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-3728.

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Kakami, Akira, Ryoma Hiyamizu, Kiyotaka Shuzenji, and Takeshi Tachibana. "Laser-assisted combustion of solid propellants." In 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-5783.

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Reports on the topic "Solid Combustion"

1

Price, E. W., and G. A. Flandro. Combustion Instability in Solid Propellant Rockets. Defense Technical Information Center, 1987. http://dx.doi.org/10.21236/ada179701.

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Branch, Melvyn C. Nonsteady Combustion Mechanisms of Advanced Solid Propellants. Defense Technical Information Center, 1997. http://dx.doi.org/10.21236/ada329767.

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Price, E. W., and R. K. Sigman. Progress on Combustion Mechanisms of Solid Propellants. Defense Technical Information Center, 1992. http://dx.doi.org/10.21236/ada248146.

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Bushnell, D. J., J. H. Canova, and A. Dadkhah-Nikoo. Municipal solid waste combustion: Fuel testing and characterization. Office of Scientific and Technical Information (OSTI), 1990. http://dx.doi.org/10.2172/7076164.

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Jones, C., J. Hahn, B. Magee, et al. Utilization of ash from municipal solid waste combustion. Office of Scientific and Technical Information (OSTI), 1999. http://dx.doi.org/10.2172/757056.

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Anthony, E. J., G. G. Ross, E. E. Berry, R. T. Hemings, R K Kissel, and C. C. Doiron. Characterization of solid wastes from circulating fluidized bed combustion. Natural Resources Canada/ESS/Scientific and Technical Publishing Services, 1989. http://dx.doi.org/10.4095/304421.

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Cameron, D. Characterization of solid wastes from conventional coal combustion processes. Office of Scientific and Technical Information (OSTI), 1989. http://dx.doi.org/10.2172/5540010.

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Cameron, D. Characterization of solid wastes from conventional coal combustion processes. Office of Scientific and Technical Information (OSTI), 1989. http://dx.doi.org/10.2172/5752711.

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Segal, Corin. Solid-Gas Interface Analyses for High Energy Density Fuels Combustion. Defense Technical Information Center, 1999. http://dx.doi.org/10.21236/ada368598.

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Derek L. Aldred and Timothy Saunders. Achieve Continuous Injection of Solid Fuels into Advanced Combustion System Pressures. Office of Scientific and Technical Information (OSTI), 2007. http://dx.doi.org/10.2172/909121.

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