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Eddy Break-Up Model for combustion
Combustion modeling is one of the most important topics in demand. Its wide range of applications has attracted the attentions of most of the researchers around the globe. In most of the combustion systems fuel and oxygen (or air) are separately supplied in the combustion chamber. Due to this chemical reaction and combustion occurs simultaneously in the combustion chamber. However, it is evident that rate of rate of chemical reaction is faster than rate of mixing of fuel and oxygen. Which interprets that rate of combustion is controlled by rate of mixing. Such cases where formation of pre-mixture is difficult are called diffusion combustion or diffusion flames. Diffusion flames can be laminar diffusion flames (eg. Candles and matches burning in the air etc.) and turbulent diffusion flames (eg. furnaces, turbo-machinery, some liquid-fuel rocket engines and internal combustion engines) depending on the nature of mixed gas flow. Further, the flame shapes of this kind of burning are divided into two categories oxygen-rich diffusion flames and oxygen-deficient. Flame shapes also depend on the discharging velocity of fuel and air. Eddies inside the air flow plays an important role in deciding the flame shapes. With increase in discharging velocity of fuel into the air laminar diffusion flames tends to become turbulent diffusion flames. This leads to an increase in the flame height and finally it gains a maximum height (critical limit). After this limit further increase in the jet velocity of the fuel adds to instability of turbulent flame. The position where laminar flame is changing into turbulent flame is termed as “break-up point”. Increase in jet velocity after critical limit results in decrease of the whole flame height. Beyond this point the height of the break-up point reaches a certain value where even after increasing the jet velocity of fuel the flame height will not change. Studies by Hawthorne et al. prove that the chemical reaction rates in turbulent diffusion flames and in laminar diffusion flames are almost similar.

Combustion plays a vital role in many applications and a proper understanding of its effect on the system can be very helpful in designing the newer technologies and improving the existing ones. Now a day, numerical modeling is a most effective tool for understanding and studying such problems. But a number of problems are associated with it such as: In this context, many combustion models are purposed. There is a big list of such models in literature but due to simplicity “The eddy break-up (EBU) model” proposed by Spalding and later modified by Magnusen and Hiertager became one among the most popular models. It is based on the assumption that the reaction rate is controlled by turbulent mixing because of the dependence of reaction rate on the mixing of the turbulent eddies. It is well documented that there are strong interactions between the turbulent flow and reactions. The heat released during the reaction affects the density and hence turbulence. While the turbulent flow induces changes concentration and temperature pulsations which enhance the mixing and heat transfer and affect the reaction rate. Turbulence also results in deformations in burning flame surface due to which folding occurs and the surface is also broken into pieces of different sizes. This enhances the total surface area of the flame and thus increases the combustible mixed gases burnt per unit time. Due to this, turbulent flames grow at a much faster rate than that of laminar flames. Therefore, Spalding (1971) defined rate of fuel consumption as a function of local flow properties of fuel and oxidant. This model is based on a single step global infinitely fast stochiometric chemical reaction.
 * The control equations associated are very complicated.
 * Large number of control equation need to be studied which include knowledge of both fluid dynamics and chemistry of chemical reactions during combustion.
 * Involvement of huge number of components in the chemical reactions.
 * There are serious time-scale problems because of mismatch in chemical reaction rate and fluid transport rate.
 * Effect of several other processes like heat transfer, radiation, convection and diffusion.

1 kg of fuel + s kg of oxidant→(1+s) kg of products

For mj as mass fraction and Mj as molecular weight of species j; local density of mixture (ρ) is dependent on concentration of reactant and products and temperature of mixture. It can be mathematically calculated as:

It is used to express the turbulent dissipation rate of fuel (Rfu), oxygen (Rox) and products (Rpr) as:

Where k is the turbulent kinetic energy,  is the rate of dissipation of k,   and   are model constants (value varies from .35 to 4). The reaction rate of fuel is considered to be smallest among all and is given by:

The model also leads to determination of mass fraction of product and oxygen using transport equation of mixture fraction (f)

For solving we need to first find the stociometric mixture fraction (fst) when there is no fuel and oxygen is present in products, which is defined as

Above equations (7-9) not only shows linear relation of mixture fraction with mass fraction of oxygen and products but also helps in predicting their values. Magnussen and Hjertager (1976) utilize this model and conformity of experimental results with predictions supports this model. Several other researchers also justified the beauty of this model for fairly good predictions which are quite close to experimental results. Hence, this model is a topic of top priority due to its simplicity, steady convergence, and implementation in CFD procedures.

References and further readings
1. Versteeg H.K. and Malalasekera W., An introduction to computational fluid dynamics, ISBN 978-81-317-2048-6.

2. Gao Y. and Chow W.K., A Brief Review on combustion modeling,International Journal on Architectural Science, Volume 6, Number 2, p.38-69, 2005.

3.Spalding D.B., Mixing and chemical reaction in steady confined turbulent flames, Thirteenth symposium (international) on combustion, The combustion institute, pp. 649-657, 1971.

4. Magnussen B.F. and Hjertager B.H., On the mathematical modeling of turbulent combustion with special emphasis on shoot formation and combustion, Sixth symposium (International) on combustion, The combustion institute, pp. 719-729, 1976