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Modeling Unsteady Phenomena in an Axial Compressor
Mathematical Models and Computer Simulations Pub Date : 2020-06-08 , DOI: 10.1134/s2070048220030187 D. V. Voroshnin , O. V. Marakueva , A. S. Muraveiko
中文翻译:
轴流压缩机中的非稳态现象建模
更新日期:2020-06-08
Mathematical Models and Computer Simulations Pub Date : 2020-06-08 , DOI: 10.1134/s2070048220030187 D. V. Voroshnin , O. V. Marakueva , A. S. Muraveiko
Abstract
The flow in a four-stage axial compressor is investigated by numerical modeling using the Numeca FINE/Turbo software. A few approaches to modeling the rotor-stator interaction are considered: the steady statement with the use of the Mixing Plane boundary condition, the fully unsteady statement (URANS), and the non-linear harmonic (NLH) method. These approaches are compared by considering the time-averaged and instantaneous integral parameters of the compressor and the pulsations of local parameters.中文翻译:
轴流压缩机中的非稳态现象建模