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Mathematical Models are the actual physical processes represented by a set of appropriate equations. The combustion process involved in the Gas turbine can be predicted using the Mathematical Modeling. The conservation of mass, momentum and Energy plays a vital role in the combustion process. Standard K-ὲ models are used to predict the reaction rate and turbulent viscosity. The main goal of this job it is to show the combustion models applied for an annular combustion chamber for small gas turbines, considering aspects about the speed, pressure and temperature, which can be used to feature the flame behavior and its effects in efficiency and pollution emission. The Alternative fuels have been chosen in such a way that the emission is low as well as good performance characteristics like conventional fuel. The performance parameters like Combustion Efficiency, Combustion Intensity, and Adiabatic flame Temperature and Mixture fraction has been obtained by using the Mathematical Modeling. Without carry out the experimental Work one can predict the Performance by using Mathematical Modeling .The Modeling is performed in MATLAB Simulink package and how the Performance parameters varies in relation with the changes in the variables like mass flow rate, initial temperature and Combustion pressure has been discussed and plotted in a effective way. The Results of various Alternative fuels have been compared effectively.

Mathematical Modeling, Investigation and comparison on the Effect of Various Alternative Fuels on the Performance of Gas Turbine Combustion Process