Combustion research currently aims to reduce emissions, whilst improving the fuel economy. Burning fuel in excess of air, or lean-burn combustion, is a promising alternative to conventional combustion, and can achieve these requirements simultaneously. However, lean-burn combustion poses new challenges, especially for internal combustion (IC) engines. Therefore, models used to predict such combustion have to be reliable, accurate and robust. In this work, the flamelet approach in the Reynolds-Averaged Navier- Stokes framework, is used to simulate flames relevant to spark-ignition IC engines. A central quantity in the current modelling approach is the scalar dissipation rate, which represents coupling between reaction and diffusion, as well as the flame front dynamics. In the first part of this thesis, the predictive ability of two reaction rate closures, viz. strained and unstrained flamelet models, are assessed through a series of experimental test cases. These cases are: spherically propagating methane- and hydrogen-air flames and combustion in a closed vessel. In addition to these models, simpler algebraic closures are also used for comparison. It is shown that the strained flamelet model can predict unconfined, spherically propagating methane-air flames reasonably well. By comparing spherical flame results with planar flames, under identical thermochemical and turbulence conditions, it is shown that the turbulent flame speed of spherical flames are 10 to 20% higher than that of planar flames, whilst the mean reaction rates are less influenced by the flame geometry. Growth of the flame brush thickness in unsteady spherical flames have been attributed to turbulent diffusion in past studies. However, the present analyses revealed that the dominant cause for this increase is the heat-release induced convective effects, which is a novel observation. Unlike methane-air flames, hydrogen-air flames have non-unity Lewis numbers. Hence, a novel two degrees of freedom approach, using two progress variables, is used to describe the thermochemistry of hydrogen-air flames. Again, it is shown that the strained flamelet model is able to predict the experimental flame growth for stoichiometric hydrogen-air flames. However, none of the models used in this work were able to predict lean hydrogen-air flames. This is because these flames are thermo-diffusively unstable and the current approach is inadequate to represent them. When combustion takes place inside a closed vessel, the compression of the end gases by the propagating flame causes the pressure to rise. This is more representative of real IC engines, where intermittent combustion takes place. The combustion models are implemented in a commercial computational fluid dynamics (CFD) code, STAR-CD, and it is shown that both strained and unstrained flamelet models are able to predict the experimental pressure rise in a closed vessel. In the final part of this work, a spark-ignition engine is simulated in STAR-CD using the flamelet model verified for simpler geometries. It is shown that this model, together with a skeletal mechanism for iso-octane, compares reasonably well with experimental cylinder pressure rise. Results obtained from this model are compared with two models available in STAR- CD. These models require some level of tuning to match the experiments, whereas the modelling approach used in this work does not involve any tunable parameters.

This thesis presents the results of an investigation of the differences in combustion between gasoline and natural gas in a spark-ignition engine. Combustion development is influenced by calorific value, specific heat, flame speed and the gaseous or liquid state of the fuel. Simple simulation programs were set up to investigate the effects of low flame speed and higher specific heat of the fuel-air mixture. Actual performance was measured on a single cylinder test engine using ionization probes as flame detectors and a pressure pick-up. The experimental results show that longer ignition delay and limited flame speed at high pressure and temperature are the main reasons for' the power loss of natural gas at high engine speed; this is in addition to the basic loss due to the replacement of air by gaseous fuel in the cylinder. From calculations, it was learned that specific heat and dissociation differences had little effect on power. / Applied Science, Faculty of / Mechanical Engineering, Department of / Graduate

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Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1981. / MICROFICHE COPY AVAILABLE IN ARCHIVES AND ENGINEERING. / Includes bibliographical references. / by Mehdi Namazian. / Ph.D.

Thesis (Ph.D.)--University of Melbourne, Dept. of Mechanical Engineering, 2009. / Typescript. Includes bibliographical references (leaves 231-245)

Call number: LD2668 .T4 1984 G666 / Master of Science

Determinação do desempenho de um motor à combustão interna com ignição por centelha, sem modificação em sua taxa de compressão volumétrica, usando álcool etílico vaporizado como combustível. Para facilidade de obtenção de dados usou-se um sistema de aquecimento elétrico para a geração do vapor do álcool etílico. Mediu-se as descargas de ar e combustível, a potência no eixo e a temperatura dos gases de escape para vários ângulos de avanço de centelha e rotações do eixo do motor. Os resultados obtidos foram comparados com o desempenho do mesmo motor funcionando com gasolina e álcool, pelo sistema de mistura usando carburador. O processo de vaporização pode ser aplicado a motores do tipo ciclo Otto , que poderão funcionar com álcool etílico ou gasolina, com poucas alterações em seu desempenho. / Performance determination of a spark-ignition combustion-engine, without modification in compression ratio, fueled with etanol vapours. The data acquisition was simplified by the use of an electric heater to generate the etanol vapours. The data acquired are flow of air and fuel, net power and escape gases temperature to various spark advance angles and engine speed. The performance was compared with those obtained with the carburator system motor, gasoline and etanol as fuel. The vaporization process will be applied in Otto cycle engines that may work with etanol or gasoline as fuels, with few performance alterations.

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