Influence of Inflow Turbulence and Distortion on a Two-Stage Low Pressure Axial Turbine at Low Reynolds Numbers
A two-stage low pressure turbine, developed by MTU Aero Engines AG (MTU), has been tested in the altitude test facility of the Institute for Aircraft Propulsion Systems (ILA) at Stuttgart University. The focus was on the change in the turbines behaviour to a rise in inflow turbulence levels and inflow distortion at flight conditions. Hence, the turbine flow with a clean inlet was compared to two cases with a built in turbulence grid prior to the first vane at a Reynolds number of 75,000. Data was collected in the inflow and inside the turbine using radial and area probe traverses. The observed rise in inflow turbulence level and the inflow distortion impacted the first turbine nozzle guide vane. Static pressure tappings and thin film gauges show changes in separation as well as transition location on the vane’s suction side. Five hole probe and 3D hot film probe measurements show distinct changes in secondary flow patterns as well as nozzle guide vane wakes. The changes lead to a higher blade row efficiency and a more homogeneous distribution of turbulence intensity at stator exit.