Bidar, O., He, P., Anderson, S. orcid.org/0000-0002-7452-5681 et al. (1 more author)
(2024)
Aerodynamic shape optimisation using a machine learning-augmented turbulence model.
In:
AIAA SCITECH 2024 Forum.
AIAA SCITECH 2024 Forum, 08-12 Jan 2024, Orlando, FL, USA.
American Institute of Aeronautics and Astronautics
ISBN 9781624107115
Abstract
This paper presents an aerodynamic shape optimisation approach that utilises machine learning techniques to augment the turbulence model for the steady-state Reynolds-averaged Navier-Stokes (RANS) simulations—which are prone to inaccuracies for complex flows involving phenomena such as separation. We employ the field inversion and machine learning (FIML) approach which infers model discrepancies by solving a number of inverse problems (for different shapes and/or flow conditions) given some high-fidelity data, and uses machine learning (such as neural networks) to generalise the discrepancy fields for unseen cases. As a proof-of-concept we use direct numerical simulation (DNS) data for a set of parameterised periodic hills to augment the two-equations k − ω SST model using FIML, then incorporating it in the CFD solver for aerodynamic shape optimisation where the cost function is the drag minimisation. To illustrate the inherent optimisation sensitivity to the choice of turbulence model, we also use the Wilcox k − ω model for comparison. Once the optimal shapes are achieved for the different turbulence models, we propose using the hybrid RANS-LES improved delayed detached eddy simulations (IDDES) to validate the flow predictions, which in turn is validated against the available DNS data. Results highlight the sensitivity of optimisation to the turbulence model in the presence of flow separation, and the FIML-augmented k −ω SST model is able to achieve much higher drag reduction (20.8 − 25.3%) with fair agreement to the IDDES predictions (in terms of velocity and skin friction). The baseline SST model achieves a drag reduction of 4.5 − 6.5%, and the velocity and skin friction compares poorly to the IDDES results.
Metadata
Item Type: | Proceedings Paper |
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Authors/Creators: |
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Copyright, Publisher and Additional Information: | © 2024 The Authors. Except as otherwise noted, this author-accepted version of a paper published in AIAA SCITECH 2024 Forum is made available via the University of Sheffield Research Publications and Copyright Policy under the terms of the Creative Commons Attribution 4.0 International License (CC-BY 4.0), which permits unrestricted use, distribution and reproduction in any medium, provided the original work is properly cited. To view a copy of this licence, visit http://creativecommons.org/licenses/by/4.0/ |
Keywords: | Machine Learning; Turbulence Models; Aerodynamic Shape Optimization; Improved Delayed Detached Eddy Simulation; Reynolds Averaged Navier Stokes; Flow Separation; Unsteady Turbulent Flow; Skin Friction; Inverse Problems; Kinematic Viscosity |
Dates: |
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Institution: | The University of Sheffield |
Academic Units: | The University of Sheffield > Faculty of Engineering (Sheffield) > Department of Mechanical Engineering (Sheffield) The University of Sheffield > Faculty of Engineering (Sheffield) > Department of Automatic Control and Systems Engineering (Sheffield) |
Depositing User: | Symplectic Sheffield |
Date Deposited: | 08 Jul 2024 14:41 |
Last Modified: | 08 Jul 2024 19:45 |
Status: | Published |
Publisher: | American Institute of Aeronautics and Astronautics |
Refereed: | Yes |
Identification Number: | 10.2514/6.2024-1231 |
Related URLs: | |
Open Archives Initiative ID (OAI ID): | oai:eprints.whiterose.ac.uk:214493 |