The challenges in designing high performance combustion systems have not changed significantly over the years, but the approach has shifted towards a more sophisticated analysis process. A technical discussion on combustion technology status and needs will show that the classic impediments that have hampered progress towards near stoichiometric combustion still exist. The paper presents the design for annular combustion chamber for annular gas turbine for 20 kW power generation wit kerosene as fuel and its also include the CFD simulation is carried out with the CFD tool ANSYS CFX. It also give results from CFD simulation of temperature distribution at centerline of liner, at liner wall and at exit of combustion chamber
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