Unsteady heat transfer in a turbine blade film cooling flow is studied using detached eddy simulation (DES). Detailed computation of a single row of 35 degree round holes on a flat plate has been obtained for a blowing ratio of 1.0 and a density ratio of 2.0. The instantaneous flow fields and heat transfer distributions are found to be highly unsteady and oscillatory in nature. The fluctuation of the adiabatic effectiveness and heat transfer coefficient, for example, can be as high as 15 and 50 percent of the time-averaged value, respectively. The correlation between the coherent vortical structures and the unsteady heat transfer is carefully examined. It is shown that the fluctuations in the adiabatic effectiveness and heat transfer coefficient are mainly caused by the spanwise fluctuation of the coolant jet and the thermal turbulent boundary layer accompanying the unsteady flow structures.
|Number of pages||12|
|Publication status||Published - 2008|
|Event||46th AIAA Aerospace Sciences Meeting and Exhibit - Reno, United States|
Duration: 07 Jan 2008 → 10 Jan 2008
|Conference||46th AIAA Aerospace Sciences Meeting and Exhibit|
|Period||07/01/2008 → 10/01/2008|
Kim, S. I., & Hassan, I. (2008). Unsteady heat transfer analysis of a film cooling flow. Paper presented at 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, United States. http://arc.aiaa.org/doi/abs/10.2514/6.2008-1287