Validation and verification of RANS solvers for TUDa-GLR-OpenStage transonic axial compressor
نویسندگان
چکیده
This paper presents a comprehensive validation and verification study of turbomachinery Reynolds-averaged Navier-Stokes flow solvers on the transonic axial compressor TUDa-GLR-OpenStage. Two commercial namely Ansys CFX Numeca FineTurbo are adopted to provide benchmark solutions, which can be used for other RANS in future. Based these solvers, five sets grids, two advection schemes (i.e., central difference second-order upwind), four turbulence models SA, SA-RC, SST EARSM) rotor-stator interface mixing plane sliding plane) investigated quantify their effects predicting performance field stage. Results show that choices grid density model most sensitive prediction, leading 5% 7% variation characteristics, respectively. Regarding choice density, method estimate discretization error is demonstrated, transferrable cases. model, EARSM found overall accurate among models, limitations deficiencies rest discussed detail based analysis mean fields eddy viscosity fields. The grids major CFD results presented this work open-accessed community further research. discussions useful reference future practices simulations compressors.
منابع مشابه
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ژورنال
عنوان ژورنال: Journal of the Global Power and Propulsion Society
سال: 2023
ISSN: ['2515-3080']
DOI: https://doi.org/10.33737/jgpps/158034