Relevant bibliographies by topics / Control of the combustion

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Control of the combustion'

Author: Grafiati
Published: 4 June 2021
Last updated: 3 February 2022

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Journal articles on the topic "Control of the combustion"

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Jackson, M. D., and A. K. Agrawal. "Active Control of Combustion for Optimal Performance." Journal of Engineering for Gas Turbines and Power 121, no. 3 (July 1, 1999): 437–43. http://dx.doi.org/10.1115/1.2818492.

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Combustion-zone stoichiometry and fuel-air premixing were actively controlled to optimize the combustor performance over a range of operating conditions. The objective was to maximize the combustion temperature, while maintaining NOx within a specified limit. The combustion system consisted of a premixer located coaxially near the inlet of a water-cooled shroud. The equivalence ratio was controlled by a variable-speed suction fan located downstream. The split between the premixing air and diffusion air was governed by the distance between the premixer and shroud. The combustor performance was characterized by a cost function evaluated from time-averaged measurements of NOx and oxygen concentrations in products. The cost function was minimized by the downhill simplex algorithm employing closed-loop feedback. Experiments were conducted at different fuel flow rates to demonstrate that the controller optimized the performance without prior knowledge of the combustor behavior.
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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 (May 31, 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 compression ignition combustion is a good parameter for combustion mode transition control when the hybrid combustion mode is used during the transition. This paper presents a control oriented model of the spark ignition–homogeneous charge compression ignition hybrid combustion mode, where the spark ignition combustion phase is modeled under the two-zone assumption and the homogeneous charge compression ignition combustion phase under the one-zone assumption. Note that the spark ignition and homogeneous charge compression ignition combustions are special cases in this combustion model. The developed model is capable of simulating engine combustion over the entire operating range, and it was implemented in a real-time hardware-in-the-loop simulation environment. The simulation results were compared with those of the corresponding GT-Power model, and good correlations were found for both spark ignition and homogeneous charge compression ignition combustions.
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Seume, J. R., N. Vortmeyer, W. Krause, J. Hermann, C. C. Hantschk, P. Zangl, S. Gleis, D. Vortmeyer, and A. Orthmann. "Application of Active Combustion Instability Control to a Heavy Duty Gas Turbine." Journal of Engineering for Gas Turbines and Power 120, no. 4 (October 1, 1998): 721–26. http://dx.doi.org/10.1115/1.2818459.

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During the prototype shop tests, the Model V84.3A ring combustor gas turbine unexpectedly exhibited a noticeable “humming” caused by self-excited flame vibrations in the combustion chamber for certain operating conditions. The amplitudes of the pressure fluctuations in the combustor were unusually high when compared to the previous experience with silo combustor machines. As part of the optimization program, the humming was investigated and analyzed. To date, combustion instabilities in real, complex combustors cannot be predicted analytically during the design phase. Therefore, and as a preventive measure against future surprises by “humming,” a feedback system was developed which counteracts combustion instabilities by modulation of the fuel flow rate with rapid valves (active instability control, AIC). The AIC achieved a reduction of combustion-induced pressure amplitudes by 86 percent. The Combustion instability in the Model V84.3A gas turbine was eliminated by changes of the combustor design. Therefore, the AIC is not required for the operation of customer gas turbines.
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Ravaglioli, Vittorio, Fabrizio Ponti, Matteo De Cesare, Federico Stola, Filippo Carra, and Enrico Corti. "Combustion Indexes for Innovative Combustion Control." SAE International Journal of Engines 10, no. 5 (September 4, 2017): 2371–81. http://dx.doi.org/10.4271/2017-24-0079.

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Paschereit, Christian Oliver, Peter Flohr, and Ephraim J. Gutmark. "Combustion Control by Vortex Breakdown Stabilization." Journal of Turbomachinery 128, no. 4 (February 1, 2002): 679–88. http://dx.doi.org/10.1115/1.2218521.

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Flame anchoring in a swirl-stabilized combustor occurs in an aerodynamically generated recirculation region which is a result of vortex breakdown (VBD). The characteristics of the recirculating flow are dependent on the swirl number and on axial pressure gradients. Coupling with downstream pressure pulsations in the combustor affects the VBD process. The present paper describes combustion instability that is associated with vortex breakdown. The mechanism of the onset of this instability is discussed. Passive control of the instability was achieved by stabilizing the location of vortex breakdown using an extended lance. The reduction of pressure pulsations for different operating conditions and the effect on emissions in a laboratory scale model atmospheric combustor, in a high pressure combustor facility, and in a full scale land-based gas-turbine are described. The flashback safety, one of the most important features of a reliable gas turbine burner, was assessed by CFD, water tests, and combustion tests. In addition to the passive stabilization by the extended lance it enabled injection of secondary fuel directly into the recirculation zone where the flame is stabilized. Tests were conducted with and without secondary fuel injection. Measurements and computations optimized the location of the extended lance in the mixing chamber. The effect of variation of the amount of secondary fuel injection at different equivalence ratios and output powers was determined. Flow visualizations showed that stabilization of the recirculation zone was achieved. Following the present research, the VBD stabilization method has been successfully implemented in engines with sufficient stability margins and good operational flexibility. This paper shows the development process from lab scale tests to full scale engine tests until the implementation into field engines.
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Corbett, N. C., and N. P. Lines. "Control Requirements for the RB 211 Low-Emission Combustion System." Journal of Engineering for Gas Turbines and Power 116, no. 3 (July 1, 1994): 527–33. http://dx.doi.org/10.1115/1.2906851.

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The RB 211 DLE series staged, premix, lean burn combustor demands total integration of control system and combustion hardware. The controls design process is described from the conception of the Engine Management System (EMS), which provides protection and control in separate environments, through to implementation of engine development testing. The process of devising an acceptable fueling strategy to each combustion stage is discussed. This identified the requirements for the computation of complex routines in order to control combustion zone temperatures. The sensitivity of the control design to external conditions of humidity, ambient temperature, and fuel composition is explored. Extensive simulation was used to determine necessary instrumentation accuracies. The paper concludes with a review of the development testing and the final control system configuration.
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SCHADOW, K. C., E. GUTMARK, and K. J. WILSON. "Active Combustion Control in a Coaxial Dump Combustor." Combustion Science and Technology 81, no. 4-6 (February 1992): 285–300. http://dx.doi.org/10.1080/00102209208951807.

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Abbondanza, Marco, Nicolò Cavina, Enrico Corti, Davide Moro, Fabrizio Ponti, and Vittorio Ravaglioli. "Development of a Combustion Delay Model in the Control of Innovative Combustions." E3S Web of Conferences 197 (2020): 06013. http://dx.doi.org/10.1051/e3sconf/202019706013.

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In modern internal combustion engines the research for innovative solutions aimed at the simultaneous reduction of engine-out pollutants and fuel consumption requires synergies from different application areas: the thermo-fluid dynamic design of the combustion chamber, the study and production of specific components for air and fuel supply, the development of sensors and related methods of analyzing their signals to control the combustion process. The most promising innovative combustion methodologies suitable to achieve high efficiency and low emissions, commonly named Low Temperature Combustions (LTC), usually require sophisticated techniques for the management of the combustion phase. With respect to the combustion angular position control, directly performed in traditional spark ignition engines through the ignition from the spark plug and in compression ignition engines by the timing of fuel injection, the ignition mechanisms of LTC combustions are characterized by a high sensitivity to the thermal conditions of the combustion chamber which greatly modifies the angular position of the combustion, mainly due to the combination of high ignition delays and lean homogeneous mixture. Once the hardware of the air and fuel supply systems has been defined, it is therefore essential to ensure the correct management of the combustion phase. In this paper a model for the estimation of the delay between the start of injection and the start of combustion is presented. The model has been developed analyzing the experimental data from a modified cylinder of a diesel engine, fueled with gasoline, while the other three cylinders were still running with Diesel fuel. This solution represents a first step that allows analyzing the behavior of the combustion of gasoline in a Diesel engine, with the final goal to inject gasoline in all the engine cylinders. In particular, the approach used is similar to the one already applied in a traditional turbocharged gasoline engine, where the goal was to estimate the time delay between the spark firing and the start of combustion, mainly to detect the presence of undesired pre-ignition due to the presence of hot spots related to slightly knocking conditions. As it is well known, the role of the pilot injection is to reduce the ignition delay of the main injection. However, to significantly accelerate the ignition of the fuel injected with the main injection, it is necessary to burn a sufficient quantity of the fuel injected by the pilot before the Top Dead Center position (TDC). The application of this model has to allow the implementation of a feed-forward control to stabilize the whole combustion process and achieve the best conversion efficiency from energy to work, taking into account the operational constraints that must be satisfied to guarantee the integrity of the engine and the compliance with the homologation rules.
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Zhao, Zhelong, and Xianyu Wu. "Control Oriented Model for Expander Cycle Scramjet." MATEC Web of Conferences 257 (2019): 01004. http://dx.doi.org/10.1051/matecconf/201925701004.

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As a efficient and simple design, expander cycle is widely applied in LRE engineering, but it is seldomly used on scramjet research. In order to establish a complete mathematical model for expander cycle scramjet, a control-oriented model for expander cycle scramjet is proposed in this paper. This model consists of four major parts: combustor, cooling channel, turbo pump and nozzle and gives the result of pressure, temperature, mach number and velocity distribution of combustor and cooling channel and is capable of simulate both pure supersonic combustion mode and supersonic shock wave mode of the combustor. Each part is given by specific mathematical description, which contains the calculation of airflow, combustion, heat transfer and thermal cracking of kerosene. By putting all these parts together, a complete model is formed. This model is proposed to calculate the performance and condition of the engine precisely, comprehensively, swiftly and can be directly used in further study.
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Yi, Tongxun, and Ephraim J. Gutmark. "Combustion Instabilities and Control of a Multiswirl Atmospheric Combustor." Journal of Engineering for Gas Turbines and Power 129, no. 1 (January 22, 2006): 31–37. http://dx.doi.org/10.1115/1.2181595.

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Thermoacoustic instability and lean blowout (LBO) are investigated experimentally in an atmospheric swirl-stabilized combustor fueled with gaseous propane. Factors affecting combustion instability are identified. Sinusoidal or steady air forcing of either the swirling air shear layer or the fuel line, with less than 1.0% of combustion air, can reduce pressure oscillations amplitude by more than 20dB. Phase-shifted close-loop air forcing of the flame can reduce the pressure oscillations amplitude by 13dB. For a constant air flow rate and air inlet temperature, initially smooth turbulent combustion exhibits relatively intense heat release oscillations with decreasing equivalence ratio, followed by a quiet state before blowout. High outer swirl intensity and a rich burning flame stabilization region can effectively extend the LBO limit.
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Dissertations / Theses on the topic "Control of the combustion"

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Strand, Carina Renée. "Catalytic combustion control." Thesis, Norges teknisk-naturvitenskapelige universitet, Institutt for kjemi, 2012. http://urn.kb.se/resolve?urn=urn:nbn:no:ntnu:diva-21120.

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A mathematical model representing the dynamic behaviour observed at the actual catalytic incineration plant at Perstorp was derived. The model equations for the two main process units, the heat exchanger and the incinerator, were based on the lumped systems approach in order to avoid using partial differential equations. The model was written in Matlab and implemented in Simulink using s-functions for the dynamic study. By analyzing the dynamic data from the actual plant, it was discovered that the possible source of the ocassional large temperature variations in the incinerator is the periodic variations in the inlet compositions, amplified the overly agressive air valve controller combined with a significant dead time. This results in oscillations due to overshooting. This behaviour was successfully reproduced using the derived model. Two possibilities for improving the control performance were investigated, both using already existing sensors and actuators. The first control improvement involved reducing the proportional gain according to the SIMC tuning rules for PI controllers. This resulted in a significant reduction in the amplitude of the oscillations in the temperatures throughout the reactor, and thus a more stable performance. Finally, cascade control was implemented using the faster-responding catalyst bed temperature for the inner loop, and the reactor outlet temperature for the outer loop. This provided the most optimal results with the best disturbance rejection as it is able to compensate for the disturbance before it is detected in the outlet temperature.
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Bhidayasiri, Roongrueng. "Control of combustion." Thesis, Imperial College London, 1998. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.286243.

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LI, GUOQIANG. "EMISSIONS, COMBUSTION DYNAMICS, AND CONTROL OF A MULTIPLE SWIRL COMBUSTOR." University of Cincinnati / OhioLINK, 2004. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1092767684.

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Fussey, Peter Michael. "Automotive combustion modelling and control." Thesis, University of Oxford, 2014. http://ora.ox.ac.uk/objects/uuid:ec66cbb1-407e-431c-bd77-e67bcf33be3a.

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This thesis seeks to bring together advances in control theory, modelling and controller hardware and apply them to automotive powertrains. Automotive powertrain control is dominated by PID controllers, look-up tables and their derivatives. These controllers have been constantly refined over the last two decades and now perform acceptably well. However, they are now becoming excessively complicated and time consuming to calibrate. At the same time the industry faces ever increasing pressure to improve fuel consumption, reduce emissions and provide driver responsiveness. The challenge is to apply more sophisticated control approaches which address these issues and at the same time are intuitive and straightforward to tune for good performance by calibration engineers. This research is based on a combustion model which, whilst simplified, facilitates an accurate estimate of the harmful NOx and soot emissions. The combustion model combines a representation of the fuel spray and mixing with charge air to give a time varying distribution of in-cylinder air and fuel mixture which is used to calculate flame temperatures and the subsequent emissions. A combustion controller was developed, initially in simulation, using the combustion model to minimise emissions during transient manoeuvres. The control approach was implemented on an FPGA exploiting parallel computations that allow the algorithm to run in real-time. The FPGA was integrated into a test vehicle and tested over a number of standard test cycles demonstrating that the combustion controller can be used to reduce NOx emissions by over 10% during the US06 test cycle. A further use of the combustion model was in the optimisation of fuel injection parameters to minimise fuel consumption, whilst delivering the required torque and respecting constraints on cylinder pressure (to preserve engine integrity) and rate of increase in cylinder pressure (to reduce noise).
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Evesque, Stéphanie Marie-Noelle. "Adaptive control of combustion oscillations." Thesis, University of Cambridge, 2001. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.620985.

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Horning, Marcus. "Feedback Control for Maximizing Combustion Efficiency of a Combustion Burner System." University of Akron / OhioLINK, 2016. http://rave.ohiolink.edu/etdc/view?acc_num=akron1459356183.

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Lundström, Mikael. "Model Based HCCI Engine Combustion Control." Thesis, KTH, Reglerteknik, 2006. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-107513.

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An Homogenous Charge Compression Ignition engine is a hybrid between a Diesel and an Otto Engine. It has good fuel efficiency, close to a Diesel engine and also very low emissions of NOX and nearly no particulate soot. Other emissions are higher but can be after treated by a catalyst. The engine has not yet been fully developed so far and lacks among others a good automatic control of the combustion angle which should be held in a small window to achieve the best performance. The objective in this thesis is to achieve fast control that can hold the combustion angle window for changes in inlet pressure, loads and engine speeds. The challenges are that the system has a delay which limits the bandwidth, the dynamics change with different working conditions and a relatively large noise amplitude. Using combustion angle as reference, valve timings as control signal and other variables as engine speed, inlet pressure and load changes as disturbances, a closed loop control system can be defined. Two control methods using different kinds of variable valve timings and three controllers for each method were designed to cover most of the working conditions. These were connected by a hybrid automaton which handles all transitions and choice of controller. The result was a fast control with a 6-8 engine cycles risetime for reference changes and it can suppress inlet pressure and load disturbances well inside the combustion window. The noise showed to be white, that is using all frequencies. To achieve both a fast control and not magnify the noise a non-linear compensation link was designed that uses less gain and bandwidth for small errors. A problem with this kind of dynamic solution is engine speed ramps which needs fast reaction times which was impossible due to the delay. A proposed solution is to use mappings from non-delayed variables to do necessary adjustments of the control signal fast enough.
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Tsai, Rong-Feng. "Sources and control of combustion oscillation." Thesis, Imperial College London, 1997. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.265120.

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Hathout, Jean-Pierre 1969. "Modeling and control of combustion instability." Thesis, Massachusetts Institute of Technology, 2000. http://hdl.handle.net/1721.1/88841.

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Zhao, Dan. "Tuned passive control of combustion instabilities." Thesis, University of Cambridge, 2009. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.611839.

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Books on the topic "Control of the combustion"

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Schindler, P. J. Municipal waste combustion assessment: Combustion control at existing facilities. Research Triangle Park, NC: U.S. Environmental Protection Agency, Air and Energy Engineering Research Laboratory, 1990.

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Schindler, P. J. Municipal waste combustion assessment: Combustion control at new facilities. Research Triangle Park, NC: U.S. Environmental Protection Agency, 1989.

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Industrial combustion pollution and control. New York: Marcel Dekker, 2004.

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Yoshida, Akira, ed. Smart Control of Turbulent Combustion. Tokyo: Springer Japan, 2001. http://dx.doi.org/10.1007/978-4-431-66985-2.

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Workshop, PREDIMOT "Predictive Control of Combustion Engines" (2006 Feldkirchen in Kärnten Austria). Predictive control of combustion engines: Predimot. Linz: Trauner, 2006.

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Hanby, V. I. Combustion and pollution control in heatingsystems. London: Springer, 1993.

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King, Rudibert, ed. Active Flow and Combustion Control 2018. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-319-98177-2.

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Zaporozhets, Artur O. Control of Fuel Combustion in Boilers. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-46299-4.

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King, Rudibert, ed. Active Flow and Combustion Control 2014. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-11967-0.

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Beggs, Thomas W. Nitrogen oxide control for stationary combustion sources. Cincinnati, OH: Office of Research and Development, U.S. Environmental Protection Agency, 1986.

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Book chapters on the topic "Control of the combustion"

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Müller, Rainer. "Neural combustion control." In Lecture Notes in Computer Science, 1101–6. Berlin, Heidelberg: Springer Berlin Heidelberg, 1997. http://dx.doi.org/10.1007/bfb0020300.

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Rao, G. Amba Prasad, and T. Karthikeya Sharma. "Alternative Combustion Concepts." In Engine Emission Control Technologies, 361–404. Includes bibliographical references and index.: Apple Academic Press, 2020. http://dx.doi.org/10.4324/9780429322228-9.

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Shoemaker, R. "Process control." In Pressurized Fluidized Bed Combustion, 449–74. Dordrecht: Springer Netherlands, 1995. http://dx.doi.org/10.1007/978-94-011-0617-7_12.

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Gale, Thomas K. "Mercury Control Using Combustion Modification." In Mercury Control, 225–40. Weinheim, Germany: Wiley-VCH Verlag GmbH & Co. KGaA, 2014. http://dx.doi.org/10.1002/9783527658787.ch13.

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Maurya, Rakesh Kumar. "Closed-Loop Combustion Control." In Mechanical Engineering Series, 483–510. Cham: Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-68508-3_9.

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Guth, Ulrich, Jens Zosel, and Pavel Shuk. "Combustion Control Sensors, Electrochemical." In Encyclopedia of Applied Electrochemistry, 230–37. New York, NY: Springer New York, 2014. http://dx.doi.org/10.1007/978-1-4419-6996-5_298.

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Albin Rajasingham, Thivaharan. "Combustion Rate Shaping Control." In Nonlinear Model Predictive Control of Combustion Engines, 313–27. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-68010-7_15.

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Isermann, Rolf. "General Combustion Engine Models." In Engine Modeling and Control, 133–271. Berlin, Heidelberg: Springer Berlin Heidelberg, 2014. http://dx.doi.org/10.1007/978-3-642-39934-3_4.

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Senior, Constance. "Mercury Behavior in Coal Combustion Systems." In Mercury Control, 109–32. Weinheim, Germany: Wiley-VCH Verlag GmbH & Co. KGaA, 2014. http://dx.doi.org/10.1002/9783527658787.ch7.

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Hendricks, E. W., and K. C. Schadow. "Recent Progress in the Implementation of Active Combustion Control." In Unsteady Combustion, 139–60. Dordrecht: Springer Netherlands, 1996. http://dx.doi.org/10.1007/978-94-009-1620-3_7.

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Conference papers on the topic "Control of the combustion"

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

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SCHADOW, K., E. GUTMARK, and K. WILSON. "Active combustion control in a coaxial dump combustor." In 26th Joint Propulsion Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-2447.

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Berntsson, Andreas W., and Ingemar Denbratt. "HCCI Combustion Using Charge Stratification for Combustion Control." In SAE World Congress & Exhibition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2007. http://dx.doi.org/10.4271/2007-01-0210.

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Abdul Jalal, R. I., T. Steffen, and A. Williams. "SI engine combustion wall thermal management potential without the presence of control limitation." In 2014 UKACC International Conference on Control (CONTROL). IEEE, 2014. http://dx.doi.org/10.1109/control.2014.6915158.

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Yu, K., K. Wilson, K. Schadow, K. Yu, K. Wilson, and K. Schadow. "Active combustion control in a liquid-fueled dump combustor." In 35th Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1997. http://dx.doi.org/10.2514/6.1997-462.

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Guidugli, Guilherme. "STOVES COMBUSTION CONTROL IMPROVEMENT." In 45º Redução / 16º Minério de Ferro / 3º Aglomeração. São Paulo: Editora Blucher, 2017. http://dx.doi.org/10.5151/2594-357x-26527.

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Daley, S. "Active control of combustion instabilities." In UKACC International Conference on Control (CONTROL '98). IEE, 1998. http://dx.doi.org/10.1049/cp:19980265.

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Hillion, M., J. Chauvin, O. Grondin, and N. Petit. "Active Combustion Control of Diesel HCCI Engine: Combustion Timing." In SAE World Congress & Exhibition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2008. http://dx.doi.org/10.4271/2008-01-0984.

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Boussouara, Karima, and Mahfoud Kadja. "COMBUSTION AND NITRIC OXIDE CONTROL IN DIESEL COMBUSTION PROCESSES." In International Symposium on Sustainable Energy in Buildings and Urban Areas, SEBUA-12. Connecticut: Begellhouse, 2012. http://dx.doi.org/10.1615/ichmt.2012.sebua-12.70.

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Arsie, Ivan, Cesare Pianese, Gianfranco Rizzo, and Gabriele Serra. "A Dynamic Model For Powertrain Simulation And Engine Control Design." In 2001 Internal Combustion Engines. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2001. http://dx.doi.org/10.4271/2001-24-0017.

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Reports on the topic "Control of the combustion"

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

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

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D. J. Seery. Lean Premixed Combustion/Active Control. US: United Technologies Corp, February 2000. http://dx.doi.org/10.2172/898338.

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Osburn, Nicholas G. Model Based Control of Combustion. Fort Belvoir, VA: Defense Technical Information Center, May 1999. http://dx.doi.org/10.21236/ada376608.

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David R. Thompson, Lawrence E. Bool, and Jack C. Chen. OXYGEN ENHANCED COMBUSTION FOR NOx CONTROL. Office of Scientific and Technical Information (OSTI), April 2004. http://dx.doi.org/10.2172/889757.

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Bool, Lawrence E., Jack C. Chen, and David R. Thompson. OXYGEN ENHANCED COMBUSTION FOR NOx CONTROL. Office of Scientific and Technical Information (OSTI), July 2000. http://dx.doi.org/10.2172/788767.

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Bool, Lawrence E., Jack C. Chen, and David R. Thompson. OXYGEN ENHANCED COMBUSTION FOR NOx CONTROL. Office of Scientific and Technical Information (OSTI), October 2000. http://dx.doi.org/10.2172/788768.

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David R. Thompson, Lawrence E. Bool, and Jack C. Chen. OXYGEN ENHANCED COMBUSTION FOR NOx CONTROL. Office of Scientific and Technical Information (OSTI), April 2001. http://dx.doi.org/10.2172/783587.

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Thompson, David R., Lawrence E. Bool, and Jack C. Chen. OXYGEN ENHANCED COMBUSTION FOR NOx CONTROL. Office of Scientific and Technical Information (OSTI), August 2002. http://dx.doi.org/10.2172/804912.

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David R. Thompson, Lawrence E. Bool, and Jack C. Chen. OXYGEN ENHANCED COMBUSTION FOR NOx CONTROL. Office of Scientific and Technical Information (OSTI), August 2003. http://dx.doi.org/10.2172/823174.

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