Hybrid RANS-LES Simulation of Rotor–Stator Interaction in a Compressor Stage Using a Grid-Adaptive Simulation Method

Abstract

Flows in compressors are extremely complex with various scales. Small-scale turbulence, middle-scale rotor-stator interaction, large-scale corner separation and tip leakage flow, should all be considered in the simulation of compressors. Recently, a new hybrid RANS-LES strategy that modifies the turbulent viscosity equation based on the Kolmogorov energy spectrum, termed the grid-adaptive simulation (GAS) method, is proposed by our group to achieve high accuracy simulation using different grid resolutions. In this study, the GAS method with the SST turbulence model is employed to simulate the rotor-stator interaction just with RANS-like grid resolution in a single-stage transonic compressor TUDa-GLR open test case. Compared with experiments and other simulation methods (including RANS and DDES methods), the GAS method can significantly improve the prediction accuracy for stall margin and radial distribution of flow parameters. An intuitive total pressure fluctuation caused by wakes is observed in the stator inlet. The particle tracking shows that the wake from the suction surface of the rotor has a strong trend to transport into the tip region of the stator. Unsteady temporal-spatial structures induced by local unsteadiness and rotor-stator interaction (RSI) are distinguished by Spectral proper orthogonal decomposition, which includes the reverse flow in the tip region of the rotor and the pressure wave generated from RSI. SPOD also found the separation of the stator on the suction side exhibits an unsteady fluctuation with a frequency of 1.6 BPF.