Academic literature on the topic 'Combustion of Fuel'

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Journal articles on the topic "Combustion of Fuel"

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Liu, Gaoling, Mingli Cui, Xulin Luo, Guodong Wang, Bowei Yao, and Xuesong Li. "Flash Boiling Combustion Performance of Ethanol Fuel in Controlled Reaction Environment." E3S Web of Conferences 598 (2024): 01010. http://dx.doi.org/10.1051/e3sconf/202459801010.

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The utilization of alternative fuels such as alcohols and ethers has received substantial attention for the purpose of carbon neutralization and replacing traditional fossil fuels. However, the combustion of pure alternative fuels, for instance, pure ethanol, is relatively more challenging due to its lower volatility and heat released. This research aims to study the combustion of pure ethanol fuel (E100) in a constant volume combustion chamber (CVCC) with optical access. Flash boiling atomization via elevating the fuel temperature is adopted to improve fuel atomization and consequential combu
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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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Liu, Aiguo, Ruiyang Fan, Qiaochu Liu, Lei Xi, and Wen Zeng. "Numerical and Experimental Study on Combustion Characteristics of Micro-Gas Turbine Biogas Combustor." Energies 15, no. 21 (2022): 8302. http://dx.doi.org/10.3390/en15218302.

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The use of biogas in land-based gas turbines for power generation is a promising approach to reducing greenhouse gases and our dependence on fossil fuels. The focus of this research was to investigate the fuel/air mixing and combustion performance in an DLE (dry low emission) type can combustor designed for a micro-gas turbine. The fuel and air mixing uniformity was studied considering the air flow characteristic and fuel injection performance through the numerical simulation. The influence of the fuel/air mixing characteristics on the combustion characteristics was studied by numerical simula
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Ambrose, M. J., R. F. Costello, and H. Schreiber. "Utility Combustion Turbine Evaluation of Coal Liquid Fuels." Journal of Engineering for Gas Turbines and Power 107, no. 3 (1985): 714–25. http://dx.doi.org/10.1115/1.3239793.

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A comprehensive field test was performed to evaluate the suitability of H-Coal middle distillate and full-range Exxon Donor Solvent (EDS) coal-derived liquids (CDLs) as utility combustion turbine fuels. A Westinghouse W251AA 26 MW combustion turbine operated by the Philadelphia Electric Company was the test engine. No. 2 petroleum distillate fuel was also fired to establish baseline data. This program was sponsored by the Electric Power Research Institute. Site modifications included a temporary CDL storage and fuel transfer system, water storage and injection equipment, an instrumented combus
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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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Du, Zhibin, Chao Chen, and Lei Wang. "Combustion characteristics of and bench test on “gasoline + alternative fuel”." Thermal Science, no. 00 (2020): 324. http://dx.doi.org/10.2298/tsci200704324d.

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In this study, an evaporative premixed constant-volume combustion system was designed for combustion of liquid fuels, compared with a traditional constant-volume firebomb. The effects of an alternative fuel of gasoline on the combustion characteristics of the laminar flame of gasoline were analyzed, and then a bench test was carried out. The results show that the addition of an alternative fuel of gasoline makes the maximum non-stretched flame propagation velocity of combusting gasoline increasingly close to that of combusting diluted mixed gas. The Markstein lengths of gasoline and ?gasoline
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Sharma, N. Y., and S. K. Som. "Influence of fuel volatility on combustion and emission characteristics in a gas turbine combustor at different inlet pressures and swirl conditions." Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy 216, no. 3 (2002): 257–68. http://dx.doi.org/10.1243/095765002320183577.

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The practical challenges in research in the field of gas turbine combustion mainly centre around a clean emission, a low liner wall temperature and a desirable exit temperature distribution for turboma-chinery applications, along with fuel economy of the combustion process. An attempt has been made in the present paper to develop a computational model based on stochastic separated flow analysis of typical diffusion-controlled spray combustion of liquid fuel in a gas turbine combustor to study the influence of fuel volatility at different combustor pressures and inlet swirls on combustion and e
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Liu, C. H., R. M. Perez-Ortiz, and J. H. Whitelaw. "Vaporizer Performance." Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science 206, no. 4 (1992): 265–73. http://dx.doi.org/10.1243/pime_proc_1992_206_126_02.

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Measured values of fuel droplet velocity, size and flux are presented for a vaporizer based on a T-shaped duct with upstream atomization by a single axial jet and by six radial jets. They were obtained for a practical range of kerosene and air flowrates and inlet air temperatures with the vaporizer in free air and in a sector of an annular combustor with combustion. Phase Doppler velocimetry was used to measure droplet velocity and size distributions and was complemented by photographic visualization of the flames within the combustor. The results obtained outside the combustor, and without co
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Kanik Mittal and Sachin Srivastava. "SCRAMJET: Future High Speed Aircraft." Acceleron Aerospace Journal 3, no. 7 (2024): 785. https://doi.org/10.61359/11.2106-2476.

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In the current era of technological advancement, the scramjet has become one of the most conventional engines for achieving supersonic speeds in aircraft. The scramjet comprises three basic components: the inlet, combustor, and nozzle. Various fuels, such as Kerosene, JP-7, JP-8, hydrocarbon-based fuels, and hydrogen, have been used in scramjets, demonstrating distinct performance characteristics. Tests have shown that hydrocarbon-fueled scramjet engines can achieve a Mach number range of 3.5 to 7, while solid-fueled scramjets have the potential to achieve combustion efficiencies of 0.7–0.9. F
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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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Dissertations / Theses on the topic "Combustion of Fuel"

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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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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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Farrow, Timipere Salome. "A fundamental study of biomass oxy-fuel combustion and co-combustion." Thesis, University of Nottingham, 2013. http://eprints.nottingham.ac.uk/27633/.

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While oxy-fuel combustion research is developing and large scale projects are proceeding, little information is available on oxy-biomass combustion and cocombustion with coal. To address this knowledge gap, this research conducted has involved comprehensive laboratory based fundamental investigation of biomass firing and co-firing under oxy-fuel conditions and compared it to conventional air firing conditions. First, TGA was employed to understand the fundamental behaviour of biomass devolatilisation, char combustion and nitrogen partitioning between volatiles and residual char. The results re
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Cuseo, James M. (James Michael). "Cold start fuel management of port-fuel-injected internal combustion engines." Thesis, Massachusetts Institute of Technology, 2005. http://hdl.handle.net/1721.1/32380.

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Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2005.<br>Includes bibliographical references (p. 64).<br>The purpose of this study is to investigate how changes in fueling strategy in the second cycle of engine operation influence the delivered charge fuel mass and engine out hydrocarbon (EOHC) emissions in that and subsequent cycles. Close attention will be paid to cycle-to-cycle interaction of the fueling strategy. It is our intent to see if residual fuel from each cycle has a predicable influence on subsequent cycle's charge mass and EOHC emissions. Th
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Königsson, Fredrik. "Advancing the Limits of Dual Fuel Combustion." Licentiate thesis, KTH, Förbränningsmotorteknik, 2012. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-96945.

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There is a growing interest in alternative transport fuels. There are two underlying reasons for this interest; the desire to decrease the environmental impact of transports and the need to compensate for the declining availability of petroleum. In the light of both these factors the Diesel Dual Fuel, DDF, engine is an attractive concept. The primary fuel of the DDF engine is methane, which can be derived both from renewables and from fossil sources. Methane from organic waste; commonly referred to as biomethane, can provide a reduction in greenhouse gases unmatched by any other fuel. The DDF
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Girgis, Elisabeth. "Fuel devolatilization in packed bed wood combustion." Thesis, University of Ottawa (Canada), 2004. http://hdl.handle.net/10393/26645.

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Packed bed combustion is the burning of solid fuel particles supported by a grate with the combustion air supplied from below. The combustion process is divided into four main stages: drying, devolatilization, volatiles combustion and char combustion. Biomasses proposed as renewal energy sources, such as wood, have a very high volatile content (&sim;80%). Therefore mechanistic models developed for the prediction of bed characteristics during biomass combustion must include devolatilization and volatile combustion stages in order to correctly predict combustion behaviour for better emissions co
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Elmedhem, Bashir A. "Modelling of liquid fuel combustion in furnaces." Thesis, University of Glasgow, 2000. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.325303.

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Goldsmith, Claude Franklin III. "Predicting combustion properties of hydrocarbon fuel mixtures." Thesis, Massachusetts Institute of Technology, 2010. http://hdl.handle.net/1721.1/59876.

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Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Chemical Engineering, 2010.<br>Cataloged from PDF version of thesis.<br>Includes bibliographical references (p. 189-201).<br>In this thesis, I applied computational quantum chemistry to improve the accuracy of kinetic mechanisms that are used to model combustion chemistry. I performed transition state theory calculations for several reactions that are critical in combustion, including a detailed analysis of the pressure dependence of these rate coefficients. I developed a new method for rapidly estimating the vibrational modes an
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Books on the topic "Combustion of Fuel"

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Brabbs, Theodore A. Fuel-rich catalytic combustion of a high density fuel. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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A, Merritt Sylvia, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Fuel-rich catalytic combustion of a high density fuel. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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Brabbs, Theodore A. Fuel-rich catalytic combustion of a high density fuel. Lewis Research Center, 1993.

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Brabbs, Theodore A. Fuel-rich catalytic combustion of a high density fuel. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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DuBeau, Robert William. An investigation of the effects of fuel composition on combustion characteristics in a T-63 combustor. Naval Postgraduate School, 1985.

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1956-, Ruiz Roberto, American Society of Mechanical Engineers. Petroleum Division., Energy-Sources Technology Conference and Exhibition (1992 : Houston, Tex.), and Fossil Fuels Combustion Symposium (4th : 1992 : Houston, Tex.), eds. Fossil fuel combustion, 1992. American Society of Mechanical Engineers, 1992.

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Puskar, John R., ed. Fuel and Combustion Systems Safety. John Wiley & Sons, Inc., 2013. http://dx.doi.org/10.1002/9781118779330.

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Programs, Ontario Ministry of Energy Municipal and Commercial. Combustion: Fuel and System Efficiencies. s.n, 1987.

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Alan, Williams. Combustion of liquid fuel sprays. Butterworths, 1989.

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Agency, International Energy. Co2 Emissions from Fuel Combustion. Organization for Economic Cooperation & Development, 2009.

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Book chapters on the topic "Combustion of Fuel"

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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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Goodger, Eric, and Ray Vere. "Fuel Combustion Performance." In Aviation Fuels Technology. Macmillan Education UK, 1985. http://dx.doi.org/10.1007/978-1-349-06904-0_8.

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Bryden, Kenneth M., Kenneth W. Ragland, and Song-Charng Kong. "Solid Fuel Combustion Mechanisms." In Combustion Engineering, 3rd ed. CRC Press, 2022. http://dx.doi.org/10.1201/b22232-18.

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Colannino, Joseph. "Fuel Flow." In Modeling of Combustion Systems, 2nd ed. CRC Press, 2025. https://doi.org/10.1201/9781003481362-7.

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Bachalo, W. D., A. Breña de la Rosa, and S. V. Sankar. "Diagnostics for Fuel Spray Characterization." In Combustion Measurements. CRC Press, 2024. http://dx.doi.org/10.1201/9781003578628-7.

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Basu, Prabir, Cen Kefa, and Louis Jestin. "Fuel and Combustion Calculations." In Mechanical Engineering Series. Springer New York, 2000. http://dx.doi.org/10.1007/978-1-4612-1250-8_3.

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Duan, Lunbo, and Dennis Lu. "Oxy-Fuel Combustion in FBRs." In Fluidized Bed Reactors for Carbon Capture. Springer Nature Singapore, 2024. https://doi.org/10.1007/978-981-96-0274-2_4.

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AbstractOxy-fuel combustion, also known as O2/CO2 combustion or oxy-fuel, is one of the most promising CO2 capture technologies for coal-fired power plants, technically or economically. Oxy-fuel combustion represents a pivotal advancement in carbon capture technologies, characterized by fuel burning in an oxygen-rich environment rather than in the air.
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Hein, K. "Fossil Fuel Utilisation." In Combustion Technologies for a Clean Environment. CRC Press, 2022. http://dx.doi.org/10.1201/9780367810597-8.

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Mishra, Debi Prasad, and Swarup Y. Jejurkar. "Burner Technology for Hydrogen Fuel." In Advances in Combustion Technology. CRC Press, 2022. http://dx.doi.org/10.1201/9781003049005-3.

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Colannino, Joseph. "Mixture Designs for Fuel Blends." In Modeling of Combustion Systems, 2nd ed. CRC Press, 2025. https://doi.org/10.1201/9781003481362-17.

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Conference papers on the topic "Combustion of Fuel"

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Corbo, P., F. E. Corcione, M. Costa, and F. Migliardini. "Fuel Processing for Hydrogen Fuel Cell Vehicles." In 2001 Internal Combustion Engines. SAE International, 2001. http://dx.doi.org/10.4271/2001-24-0031.

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Stuttaford, Peter J. "Alternative Fuel Considerations for Gas Turbine Combustion." In ASME Turbo Expo 2007: Power for Land, Sea, and Air. ASMEDC, 2007. http://dx.doi.org/10.1115/gt2007-27549.

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Gas turbines have the advantage of being able to operate on a wide range of fuels. Given the escalating cost of conventional fuel sources such as natural gas, there is increasing interest in, and implementation of, systems burning lower cost fuel gases. There are significant combustor performance effects when utilizing different fuels. Flame stability, emissions, durability, and combustion dynamics are critical combustion parameters which must be controlled when varying fuel constituents. Significant emphasis continues to be placed on the use of liquefied natural gas (LNG) as well as syngas de
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Pan, Gang, Hongtao Zheng, Chunliang Zhou, and Zhijia Song. "Numerical Research on Dual Fuel Combustor Combustion Performance." In ASME 2013 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/imece2013-62435.

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In order to operate with reformed gas and oil, one gas turbine combustor which burned oil was modified and a dual fuel nozzle was developed. The CFD software FLUENT was applied to study the combustion flow field of the dual fuel combustor. The PDF (Probability Density Function) model, realizable k-ε turbulence model, DPM (Discrete Phase Model), NOX model and SIMPLE (Semi Implicit Method for Pressure Linked Equations) algorithm were adopted. In this study, the enthalpy of the two fuels which entered the combustor kept constant. The parameters of combustor temperature filed, gas temperature near
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Giannini, Nicola, Alessandro Zucca, Christian Romano, and Gianni Ceccherini. "Extending the Fuel Flexibility From Natural Gas to Low-LHV Fuel: Test Campaign on a Low-NOx Diffusion Flame Combustor." In ASME Turbo Expo 2008: Power for Land, Sea, and Air. ASMEDC, 2008. http://dx.doi.org/10.1115/gt2008-50647.

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Today’s Oil &amp; Gas facility market requires enlarging machines’ fuel flexibility toward two main directions: on the one hand burning fuels with high percentages of Ethane, Butane and Propane, on the other hand burning very lean fuels with a high percentage of inerts. GE has extensive experience in burning a variety of gas fuels and blends in heavy-duty gas turbines. From a technical point of view, the tendency towards leaner fuel gases for feeding gas turbines, introduces potential risks related to combustion instability, on both combustion hardware and machines’ operability. GE Oil&amp;Gas
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Kuleshov, Andrey, Khamid Mahkamov, Andrey Kozlov, and Yury Fadeev. "Simulation of Dual-Fuel Diesel Combustion With Multi-Zone Fuel Spray Combustion Model." In ASME 2014 Internal Combustion Engine Division Fall Technical Conference. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/icef2014-5700.

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There is increasing interest in application of various alternative fuels in marine diesel engines, including methanol. One of the challenges in the relevant research is the development of computer codes for simulation of the dual-fuel working process and engineering optimization of engines. In this work the mathematical model is described which simulates a mixture formation and combustion in an engine with a dual-fuel system, in which methanol is used as main fuel and a pilot portion of diesel oil is injected to ignite methanol. The developed combustion model was incorporated into the existing
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Poyyapakkam, Madhavan, John Wood, Steven Mayers, Andrea Ciani, Felix Guethe, and Khawar Syed. "Hydrogen Combustion Within a Gas Turbine Reheat Combustor." In ASME Turbo Expo 2012: Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/gt2012-69165.

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This paper describes a novel lean premixed reheat burner technology suitable for Hydrogen-rich fuels. The inlet temperature for such a combustor is very high and reaction of the fuel/oxidant mixture is initiated through auto-ignition, the delay time for which reduces significantly for Hydrogen-rich fuels in comparison to natural gases. Therefore the residence time available for premixing within the burner is reduced. The new reheat burner concept has been optimized to allow rapid fuel/oxidant mixing, to have a high flashback margin and to limit the pressure drop penalty. The performance of the
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Tecce, Luigi, and Gaetano Continillo. "Detailed dynamical model of an on-board fuel processor for hybrid vehicles powered by Fuel Cells." In 2001 Internal Combustion Engines. SAE International, 2001. http://dx.doi.org/10.4271/2001-24-0032.

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Kinoshita, Y., J. Kitajima, M. Shiraha, and A. Tatara. "Combustion Study on Methane-Fuel Laboratory Scaled Ram Combustor." In ASME 1992 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1992. http://dx.doi.org/10.1115/92-gt-413.

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Fundamental flameholding and combustion tests using simple V-gutters for the flame holders were investigated in order to obtain basic design data of a natural gas fueled ram combustor. Then Laboratory Scaled Ram Combustor (LSRC) was designed and fabricated in the first phase of the HYPR project using the fundamental flameholding and combustion tests results. Various tests were conducted to study combustion performance, such as flame stabilization, combustion efficiency, pressure loss and so on, of the LSRC at the simulated conditions of flight Mach number 3. The results indicate that high comb
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Zheng, Hongtao, Yong Mu, and Hongjuan He. "Numerical Simulation of Combustion Flows in Dual-fuel Combustor." In 2010 Asia-Pacific Power and Energy Engineering Conference. IEEE, 2010. http://dx.doi.org/10.1109/appeec.2010.5449465.

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Deng, Yangbo, Xi Jiang, and Fengmin Su. "Combustion Characteristics of Advanced Vortex Combustor Burning H2 Fuel." In ASME 2014 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/imece2014-37475.

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The combustion characteristics of the advanced vortex combustor (AVC) burning H2 fuel are studied numerically. First, using the 19-step reaction mechanism, the flame morphology of the pre-mixed H2/Air combustion under the different conditions, is computed. The calculation results are in agreement with experimental data from the literature. Second, a numerical model of a lean premixed H2/Air combustion is set up, based on the 19-step reaction mechanism. A numerical simulation is carried out to study the combustion characteristics of the AVC. The results show that the combustion can be steadily
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Reports on the topic "Combustion of Fuel"

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Glassman, Irvin. Fuels Combustion Research, Supercritical Fuel Pyrolysis. Defense Technical Information Center, 1998. http://dx.doi.org/10.21236/ada353435.

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Swartzbaugh, Joseph. Advanced Fuel Development and Fuel Combustion. Defense Technical Information Center, 1997. http://dx.doi.org/10.21236/ada344488.

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Chow, O. K., R. L. Patel, and A. A. Levasseur. Combustion and fuel characterization of coal-water fuels. Office of Scientific and Technical Information (OSTI), 1987. http://dx.doi.org/10.2172/6471577.

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Beal, H. R., G. W. Gralton, T. W. Gronauer, G. N. Liljedahl, and B. F. Love. Combustion and fuel characterization of coal-water fuels. Office of Scientific and Technical Information (OSTI), 1987. http://dx.doi.org/10.2172/6327743.

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Chow, O. K., J. F. Durant, B. F. Griffith, L. S. Miemiec, A. A. Levasseur, and B. C. Teigen. Combustion and fuel characterization of coal-water fuels. Office of Scientific and Technical Information (OSTI), 1987. http://dx.doi.org/10.2172/6505639.

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Lachowicz, Y. V., and R. C. LaFlesh. Combustion and fuel characterization of coal-water fuels. Office of Scientific and Technical Information (OSTI), 1987. http://dx.doi.org/10.2172/6778078.

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Chow, O. K., G. W. Gralton, Y. V. Lachowicz, R. C. Laflesh, A. A. Levasseur, and G. N. Liljedahl. Combustion and fuel characterization of coal-water fuels. Office of Scientific and Technical Information (OSTI), 1989. http://dx.doi.org/10.2172/6778092.

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Zabarnick, S., J. S. Ervin, M. J. DeWitt, et al. Advanced Integrated Fuel/Combustion Systems. Defense Technical Information Center, 2004. http://dx.doi.org/10.21236/ada430732.

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Duvvuri, Tirumalesa. Liquid Metal Fuel Combustion Mechanics. Defense Technical Information Center, 1990. http://dx.doi.org/10.21236/ada230648.

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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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Abstract:
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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