期刊名称：International Journal of Innovative Research in Science, Engineering and Technology
印刷版ISSN：2347-6710
电子版ISSN：2319-8753
出版年度：2016
卷号：5
期号：4
页码：6503
DOI：10.15680/IJIRSET.2016.0504259
出版社：S&S Publications
摘要：Combustor in a Combustion system plays a vital role in controlling pressure loss distribution, durability, stability and performance. The design of combustion chamber involves complex coupling of aerodynamics, thermodynamics and chemical kinetics of reaction. There are various parameters which decide the successful design of combustion chamber, one of them is the exit profile factor or pattern factor. The life of turbine blade is decided by the exit temperature profile; hence it is vital key to be studied. In this project three different designs will be consider with some modifications implemented based on the result of different cases are simulated upto better exit temperature profile results. Therefore for every point we are trying to optimize the temperature profile at the exit.CFD tool will be extensively being used for studying this purpose. CAD tool (CATIA V5) will be used to modify the combustion chamber, Later geometry will be meshed using GAMBIT and subsequently submitted to CFD solver FLUENT so as to get the flow field result.
