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LES VALIDATION FOR A ROTATING CYLINDRICAL CAVITY WITH RADIAL INFLOW
Conference proceeding

LES VALIDATION FOR A ROTATING CYLINDRICAL CAVITY WITH RADIAL INFLOW

Michel Onori, Dario Amirante, Nicholas J. Hills and John W. Chew
ASME Turbo Expo 2016, Turbomachinery Technical Conference and Exposition, Vol.2, p.V02DT44A008/1
01/01/2016

Abstract

Engineering Engineering, Mechanical Science & Technology Technology
This paper describes Large-Eddy Simulations (LES) of the flow in a rotating cavity with narrow inter-disc spacing and a radial inflow introduced from the shroud. Simulations have been conducted using a compressible, unstructured, finite-volume solver; and testing different sub grid scale models. These include the standard Smagorinsky model with Van Driest damping function near the wall, the WALE model and the implicit LES procedure. Reynolds averaged Navier-Stokes (RANS) results, based on the Spalart-Allmaras and SST k - omega models, are also presented. LES solutions reveal a turbulent source region, a laminar oscillating core with almost zero axial and radial velocity and turbulent Ekman type boundary layers along the discs. Validations are carried out against the experimental data available from the study of Firouzian et al. [1]. It is shown that the tangential velocity and the pressure drop across the cavity are very well predicted by both RANS and LES, although significant differences are observed in the velocity profiles within the boundary layers.

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