Data-driven optimisation of closure coefficients of a turbulence model
Data-driven optimisation of closure coefficients of a turbulence model
The solution of the Reynolds-averaged Navier-Stokes equations employs an appropriate set of equations for the turbulence modelling. The closure coefficients of the turbulence model were calibrated using empiricism and arguments of dimensional analysis. These coefficients are considered universal, but there is no guarantee this property applies to test cases other than those used in the calibration process. This work aims at revisiting the universality of the closure coefficients of the original Spalart-Allmaras turbulence model using machine learning, adaptive design of experiments and accessing a high-performance computing facility. The automated calibration procedure is carried out once for a transonic, wall-bounded flow around the RAE 2822 aerofoil. It was found that: a) an optimal set of closure coefficients exists that minimises numerical deviations from experimental data; b) the improved prediction accuracy of the calibrated turbulence model is consistent across different flow solvers; and c) the calibrated turbulence model outperforms slightly the standard model in analysing complex flow features around the ONERA M6 wing. A by-product of this study is a fully calibrated turbulence model that leverages on current state-of-the-art computational techniques, overcoming inherent limitations of the manual fine-tuning process.
Council of European Aerospace Societies
Da Ronch, Andrea
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Panzeri, Marco
fed63647-8c57-4432-9622-3c1269c0eedd
Drofelnik, Jernej
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d'Ippolito, Roberto
ab8a3511-6ce5-4c0f-8623-1fb1766a61b5
2017
Da Ronch, Andrea
a2f36b97-b881-44e9-8a78-dd76fdf82f1a
Panzeri, Marco
fed63647-8c57-4432-9622-3c1269c0eedd
Drofelnik, Jernej
e785f695-61ef-4afc-bf0a-9dc7966f5516
d'Ippolito, Roberto
ab8a3511-6ce5-4c0f-8623-1fb1766a61b5
Da Ronch, Andrea, Panzeri, Marco, Drofelnik, Jernej and d'Ippolito, Roberto
(2017)
Data-driven optimisation of closure coefficients of a turbulence model.
In Aerospace Europe 6th CEAS Conference.
Council of European Aerospace Societies.
13 pp
.
Record type:
Conference or Workshop Item
(Paper)
Abstract
The solution of the Reynolds-averaged Navier-Stokes equations employs an appropriate set of equations for the turbulence modelling. The closure coefficients of the turbulence model were calibrated using empiricism and arguments of dimensional analysis. These coefficients are considered universal, but there is no guarantee this property applies to test cases other than those used in the calibration process. This work aims at revisiting the universality of the closure coefficients of the original Spalart-Allmaras turbulence model using machine learning, adaptive design of experiments and accessing a high-performance computing facility. The automated calibration procedure is carried out once for a transonic, wall-bounded flow around the RAE 2822 aerofoil. It was found that: a) an optimal set of closure coefficients exists that minimises numerical deviations from experimental data; b) the improved prediction accuracy of the calibrated turbulence model is consistent across different flow solvers; and c) the calibrated turbulence model outperforms slightly the standard model in analysing complex flow features around the ONERA M6 wing. A by-product of this study is a fully calibrated turbulence model that leverages on current state-of-the-art computational techniques, overcoming inherent limitations of the manual fine-tuning process.
Text
CEAS 2017 912 Full Paper v11
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Published date: 2017
Venue - Dates:
Aerospace Europe 6th CEAS Conference, , Bucharest, Romania, 2017-10-16 - 2017-10-20
Identifiers
Local EPrints ID: 426762
URI: http://eprints.soton.ac.uk/id/eprint/426762
PURE UUID: 5c5557cc-10be-4c1d-a896-060403a2fb4f
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Date deposited: 11 Dec 2018 17:37
Last modified: 16 Mar 2024 04:15
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Contributors
Author:
Marco Panzeri
Author:
Jernej Drofelnik
Author:
Roberto d'Ippolito
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