Bidar, O., He, P., Anderson, S. orcid.org/0000-0002-7452-5681 et al. (1 more author) (2022) Turbulent mean flow reconstruction based on sparse multi-sensor data and adjoint-based field inversion. In: AIAA AVIATION 2022 Forum. AIAA AVIATION 2022 Forum, 27 Jun - 01 Jul 2022, Chicago, IL, USA (and online). AIAA Aviation Forum Proceedings . American Institute of Aeronautics and Astronautics
Abstract
There is significant interest in using limited, experimentally measurable, data to reconstruct turbulent mean flows. One approach to achieve this is field inversion, which involves introducing a spatially varying field in the transport equation of the turbulence model, and optimising this field such that the error between the data and model predictions is minimised. This highly dimensional inverse problem is solved with gradient-based optimisation, driven by efficient derivative computations of the cost function using the adjoint method. It has been used to achieve promising results using limited observations from one data source, such as lift force, surface friction etc. In practice, experimental data are often disparate in nature: various quantities from different parts of the flow domain, with varying dimensions and quality. In this work, we will investigate the use of field inversion with disparate data based on sensor fusion and the solution of a multi-objective optimisation, for augmenting the Spalart–Allmaras turbulence model. The separated flows over the NASA wall-mounted hump and the periodic hill are used as test cases, with datasets comprising of velocity profiles, surface pressure, and surface friction. Results highlight improved mean flow reconstruction when incorporating multiple quantities.
Metadata
Item Type: | Proceedings Paper |
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Authors/Creators: |
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Copyright, Publisher and Additional Information: | © 2022 by Omid Bidar. Published by the American Institute of Aeronautics and Astronautics, Inc.. This is an author-produced version of a paper subsequently published in AIAA AVIATION 2022 Forum. Uploaded in accordance with the publisher's self-archiving policy. |
Keywords: | Sensor Fusion; Flow Characteristics; Spalart Allmaras Turbulence Model; Flow Conditions; Inverse Problems; Lift Forces; Reynolds Averaged Navier Stokes; Flow Separation; Skin Friction; Computational Fluid Dynamics |
Dates: |
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Institution: | The University of Sheffield |
Academic Units: | The University of Sheffield > Faculty of Engineering (Sheffield) > Department of Automatic Control and Systems Engineering (Sheffield) |
Funding Information: | Funder Grant number Engineering and Physical Sciences Research Council n/a |
Depositing User: | Symplectic Sheffield |
Date Deposited: | 08 Jul 2022 10:38 |
Last Modified: | 04 Aug 2022 10:51 |
Status: | Published |
Publisher: | American Institute of Aeronautics and Astronautics |
Series Name: | AIAA Aviation Forum Proceedings |
Refereed: | Yes |
Identification Number: | 10.2514/6.2022-3900 |
Related URLs: | |
Open Archives Initiative ID (OAI ID): | oai:eprints.whiterose.ac.uk:188729 |