Adjoint-based surrogate modelling of Spalart-Allmaras turbulence model using gradient enhanced kriging
Adjoint-based surrogate modelling of Spalart-Allmaras turbulence model using gradient enhanced kriging
A Gradient Enhanced Kriging algorithm has been developed to find a surrogate model of a Reynolds-Averaged Navier-Stokes solver in low speed separated flow. The surrogate relies on gradients of the modelling quantities with respect to the design parameters. The gradients are obtained using a discrete adjoint solver and are used in the surrogate model to make more accurate predictions of the full order system. Adaptive sampling accelerates the generation of the surrogate model and ensures full system dynamics are captured in regions of high nonlinearity. It is proposed that, once the model has fully developed, it can be used to fine-tune the coefficients of the Spalart-Allmaras turbulence model to minimize the error between computational results and results from higher fidelity solvers or experiments, and therefore obtain parameters which are calibrated for solving separated flows.
Aerospace Research Central
Bagheri, Amir K.
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Da Ronch, Andrea
a2f36b97-b881-44e9-8a78-dd76fdf82f1a
Bagheri, Amir K.
1cd33839-83df-4b80-8a17-98d470341c88
Da Ronch, Andrea
a2f36b97-b881-44e9-8a78-dd76fdf82f1a
Bagheri, Amir K. and Da Ronch, Andrea
(2020)
Adjoint-based surrogate modelling of Spalart-Allmaras turbulence model using gradient enhanced kriging.
In AIAA AVIATION 2020 FORUM.
Aerospace Research Central..
(doi:10.2514/6.2020-2991).
Record type:
Conference or Workshop Item
(Paper)
Abstract
A Gradient Enhanced Kriging algorithm has been developed to find a surrogate model of a Reynolds-Averaged Navier-Stokes solver in low speed separated flow. The surrogate relies on gradients of the modelling quantities with respect to the design parameters. The gradients are obtained using a discrete adjoint solver and are used in the surrogate model to make more accurate predictions of the full order system. Adaptive sampling accelerates the generation of the surrogate model and ensures full system dynamics are captured in regions of high nonlinearity. It is proposed that, once the model has fully developed, it can be used to fine-tune the coefficients of the Spalart-Allmaras turbulence model to minimize the error between computational results and results from higher fidelity solvers or experiments, and therefore obtain parameters which are calibrated for solving separated flows.
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e-pub ahead of print date: 8 June 2020
Venue - Dates:
AIAA 2020 Aviation Forum, Virtual, 2020-06-15 - 2020-06-19
Identifiers
Local EPrints ID: 484017
URI: http://eprints.soton.ac.uk/id/eprint/484017
PURE UUID: 676759e0-4495-47c7-b696-d88434929493
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Date deposited: 09 Nov 2023 17:31
Last modified: 18 Mar 2024 03:25
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Author:
Amir K. Bagheri
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