Investigation of Using High‐Order Discontinuous Galerkin Methods in Adjoint Gradient‐Based 3D Aerodynamic Shape Optimization

ABSTRACT Based on recent work by He et al. ( Computer Physics Communications 286 (2023): 108660), this work develops a robust and efficient workflow for 3D aerodynamic shape optimization (ASO) based on the discontinuous Galerkin method (DGM) with solution remapping technique. It is theoretically found and numerically validated through 2D cases that the DGMs can provide more precise adjoint‐enabled gradients even on a coarse mesh as compared with the FVMs under coequal computational costs. A number of 2D and 3D intricate cases are tested to illustrate the potential advantages of the DGM‐based ASO workflow in terms of computational efficiency and final optimization results. The results demonstrate that the solution remapping technique can save around of the computational time. Moreover, the DGM‐based workflow extends the capability to explore the design space, leading to aerodynamic shapes with superior performance.

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Publication Details

Journal
International Journal for Numerical Methods in Engineering
Published
2025-04-21
DOI
https://doi.org/10.1002/nme.70033
Primary Topic
Computational Fluid Dynamics and Aerodynamics
Type
article
Field-Weighted Citation Impact
0.00

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article

Investigation of Using High‐Order Discontinuous Galerkin Methods in Adjoint Gradient‐Based 3D Aerodynamic Shape Optimization

Kun Wang, Tiegang Liu, Yiwei Feng, Bangcheng Ai et al.
International Journal for Numerical Methods in Engineering
Computational Fluid Dynamics and Aerodynamics
article

Investigation of Using High‐Order Discontinuous Galerkin Methods in Adjoint Gradient‐Based 3D Aerodynamic Shape Optimization

Kun Wang, Tiegang Liu, Yiwei Feng, Bangcheng Ai, Lili Lv
article en

Abstract

ABSTRACT Based on recent work by He et al. ( Computer Physics Communications 286 (2023): 108660), this work develops a robust and efficient workflow for 3D aerodynamic shape optimization (ASO) based on the discontinuous Galerkin method (DGM) with solution remapping technique. It is theoretically found and numerically validated through 2D cases that the DGMs can provide more precise adjoint‐enabled gradients even on a coarse mesh as compared with the FVMs under coequal computational costs. A number of 2D and 3D intricate cases are tested to illustrate the potential advantages of the DGM‐based ASO workflow in terms of computational efficiency and final optimization results. The results demonstrate that the solution remapping technique can save around of the computational time. Moreover, the DGM‐based workflow extends the capability to explore the design space, leading to aerodynamic shapes with superior performance.

International Journal for Numerical Methods in EngineeringVol. 126(8)
China Aerodynamics Research and Development Center (CN), Beihang University (CN)
National Natural Science Foundation of China, China Postdoctoral Science Foundation, National Numerical Wind Tunnel Project of China
Openalex Percentile: Top 90%
Computational Fluid Dynamics and Aerodynamics
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