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This article is cited in 2 scientific papers (total in 2 papers)
Modeling of unsteady phenomena in an axial compressor
D. Voroshnin, O. Marakueva, A. Muraveiko NUMECA Russia, St. Petersburg
Abstract:
The flow modeling in a four-stage axial compressor is performed using Numeca FINE/Turbo software. A few approaches to a rotor-stator interaction modeling are considered: steady state with Mixing Plane, full unsteady URANS, non-linear harmonic method NLH. Time averaged and instantaneous parameters predicted by different methods are compared.
Keywords:
NLH, URANS, compressor, unsteady gasdynamic, rotor-stator interaction, computational fluid dynamics, Navier–Stokes, turbomachines.
Received: 04.03.2019 Revised: 25.06.2019 Accepted: 01.07.2019
Citation:
D. Voroshnin, O. Marakueva, A. Muraveiko, “Modeling of unsteady phenomena in an axial compressor”, Matem. Mod., 31:10 (2019), 87–97; Math. Models Comput. Simul., 12:3 (2020), 413–421
Linking options:
https://www.mathnet.ru/eng/mm4120 https://www.mathnet.ru/eng/mm/v31/i10/p87
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Abstract page: | 210 | Full-text PDF : | 107 | References: | 29 | First page: | 8 |
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