Geodesic
Modeling of unsteady phenomena in an axial compressor
Matematičeskoe modelirovanie, Tome 31 (2019) no. 10, pp. 87-97.

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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, unsteady gasdynamic, rotor-stator interaction, computational fluid dynamics, Navier–Stokes
Mots-clés : URANS, compressor, turbomachines. 
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D. Voroshnin; O. Marakueva; A. Muraveiko. Modeling of unsteady phenomena in an axial compressor. Matematičeskoe modelirovanie, Tome 31 (2019) no. 10, pp. 87-97. http://geodesic.mathdoc.fr/item/MM_2019_31_10_a7/

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