The book "Combustor Aerodynamics Study" provides a comprehensive analysis of the aerodynamic characteristics of micro gas turbine burners. It combines numerical simulations and experimental measurements to convey a deep understanding of the flow dynamics that are crucial for the efficient mixing of fuel and air. By employing Particle Image Velocimetry, detailed flow structures were captured on a laboratory model, which is significant for optimizing burner geometry and validating numerical models. The simulations, based on the Reynolds-Averaged Navier-Stokes (RANS) code, investigate the three-dimensional, viscous, and turbulent flow features of the burner model. The results reveal complex flow structures, including vortices and recirculation zones, and offer valuable insights into the operation of combustion chambers.