The Influence of the TCS on the Circumferential Mode Distribution in the Inlet of a Fanrig (UFFA)
Sophisticated noise testing of an aero engine fan on a static indoor test bed requires special arrangements to produce reliable data. One of these items used to improve the measured data quality is the TCS (turbulence control screen) (also called ICD, inlet control device). The TCS reduces the disturbances in the inflow resulting from the static conditions. In this way the results are comparable to flight tests with a more uniform inflow. The effects of the TCS with regards to turbulence structures in general are well studied. To get the full picture of the acoustic behaviour of the TCS the mode generation needs to be investigated and understood. This paper gives an overview of the inlet mode analysis performed for the UFFA (Universal Fan Facility for Acoustics). As expected the noise characteristic shows a significant difference especially upstream of the fan whether measurements were carried out with or without TCS. To get a better understanding of what is happening, the circumferential mode distribution in the inlet was measured with a CMD (circumferential mode detection) ring and the measurements were analysed with an algorithm based on the information published by the NLR (National Aerospace Laboratory of the Netherlands). The results show, that the inflow has a considerable influence on the spinning modes caused by the rotor-stator interaction (RSI) described by Tyler-Sofrin as well as on the rotor-alone noise. The circumferential modes generated by the rotor-stator interaction are significantly reduced by an unsteady nonuniform inflow while the rotor self noise is increased through turbulence-rotor interaction.