Three-dimensional calculations of the flow field around a turbine blade with film cooling injection near the leading edge

Injection of coolant air from a showerhead injection system at the leading edge of a high pressure turbine blade is investigated using a fully implici t three-dimensional finite-volume method on multi-block grids. For various blowing rates, the calculation results for the velocity and pressure fields and turbulence intensity are compared with available experimental data. Th e present method yields excellent agreement with the experiments for the is entropic Mach number distributions on the blade surface. The standard k-eps ilon turbulence model with wall functions is already capable of capturing t he major details of the flow field including the injection-induced secondar y-flow vortices, particularly so on the suction side. On the pressure side, however, the lateral jet spreading is underpredicted somewhat together wit h an exaggeration of the near-wall sink-flow vortices. On this side with co nvex walls, where turbulence anisotropy is appreciable according to the exp eriments, overall better predictions were obtained with the anisotropy corr ection of Bergeles et al. [23] promoting the Reynolds stress in the lateral direction. The correction has no beneficial effect on the suction side wit h concave walls where the turbulence anisotropy was observed to be much sma ller.