Numerical Investigation of the Aerodynamic and Thermal Behavior of a Flow Around the Blades of an Axial Gas Turbine

Gas turbines have emerged as integral components in various industrial applications, particularly in the generation of electrical power. The widespread adoption of gas turbines has sparked increased interest among researchers and designers to explore and enhance various aspects of this machinery. This study is dedicated to simulating the flow of compressible transonic fluid through a configuration of eight blades, akin to those found in gas turbines. The primary objective is to analyze and determine the pressure and temperature distribution surrounding each blade. The configuration under investigation aligns with the one previously studied by T. Arts through experimental means. The numerical results generated by the Fluent code will be examined and discussed, shedding light on the intricacies of fluid dynamics within this specific turbine blade arrangement. This research aims to contribute valuable insights for further refining the performance and efficiency of gas turbines in practical applications.