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O'Mahoney, TSD, Hills, Nicholas, Chew, John and Scanlon, T (2010) LARGE-EDDY SIMULATION OF RIM SEAL INGESTION In: ASME Turbo Expo 2010, 2010-06-14 - 2010-06-18, Glasgow, SCOTLAND.

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Unsteady flow dynamics in turbine rim seals are known to be complex and attempts accurately to predict the interaction of the mainstream flow with the secondary air system cooling flows using CFD with RANS turbulence models have proved difficult. In particular, published results from RANS models have overpredicted the sealing effectiveness of the rim seal, although their use in this context continues to be common. Previous authors have ascribed this discrepancy to the failure to model flow structures with a scale greater than can be captured in the small sector models typically used. This paper presents results from a series of Large-Eddy Simulations (LES) of a turbine stage including a rim seal and rim cavity for, it is believed by the authors, the first time. The simulations were run at a rotational Reynolds number Reθ = 2.2 × 106 and a main annulus axial Reynolds number Rex = 1.3 × 106 and with varying levels of coolant mass flow. Comparison is made with previously published experimental data and with unsteady RANS simulations. The LES models are shown to be in closer agreement with the experimental sealing effectiveness than the unsteady RANS simulations. The result indicates that the previous failure to predict rim seal effectiveness was due to turbulence model limitations in the turbine rim seal flow. Consideration is given to the flow structure in this region.

Item Type: Conference or Workshop Item (Conference Paper)
Divisions : Surrey research (other units)
Authors :
O'Mahoney, TSD
Scanlon, T
Date : 1 January 2010
Copyright Disclaimer : Copyright © 2010 by Rolls-Royce plc
Contributors :
Uncontrolled Keywords : Science & Technology, Physical Sciences, Technology, Thermodynamics, Engineering, Mechanical, Engineering, FLOW, TURBINE
Related URLs :
Depositing User : Symplectic Elements
Date Deposited : 19 Jul 2017 16:53
Last Modified : 23 Jan 2020 13:03

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