DNS of a subsonic jet on a heated curved surface
We use DNS to analyze the cooling of a heated curved surface due to a cold subsonic impinging jet. The configuration resembles several industrial applications such as impingement cooling in gas turbine blade. The ratio between the distance from the nozzle (H) and the jet diameter (D) is equal to 5. The results in terms of velocity, turbulence and heat transfer are compared with a reference simulation with where a subsonic jet impingesing on a flat surface. The results allowed to assess the influence of the curvature on the velocity and Nusselt number distribution is assessed.