TY - JOUR
T1 - A physics-constrained multi-objective CFD-driven model training framework and its application to SWTBLI flows
AU - Tang, Denggao
AU - Yi, Chen
AU - Zhang, Xin
AU - Li, Yao
AU - Yan, Chao
N1 - Publisher Copyright:
© 2025 Elsevier Masson SAS
PY - 2026/1
Y1 - 2026/1
N2 - With growing interest in data-driven turbulence modeling, field inversion and symbolic regression (FISR) have gained attention for producing interpretable correction terms. However, classical FISR lacks fully model-consistent training, limiting predictive accuracy. This study proposes a physics-constrained, multi-objective computational fluid dynamics (CFD)-driven training framework that integrates a CFD solver into gene expression programming for model-consistent training. Correction domains of symbolic expressions are constrained using inversion fields to improve interpretability. The framework is applied to a supersonic compression corner flow using the shear-stress transport (SST) model, yielding the SST-MO model. After appropriate analysis and modification, SST-MO is evaluated on a range of shock-wave/turbulent boundary-layer interaction flows across various Mach numbers, as well as a flat-plate boundary layer to assess its behavior in zero pressure gradient conditions. Classical FISR and single-objective CFD-driven methods are also tested for comparison. Results show that the proposed framework produces a correction model that balances interpretability and predictive performance. Compared to FISR, SST-MO offers improved accuracy, and it maintains greater interpretability than single-objective approaches. The results highlight the potential of multi-objective, physics-informed training for developing practical turbulence model corrections.
AB - With growing interest in data-driven turbulence modeling, field inversion and symbolic regression (FISR) have gained attention for producing interpretable correction terms. However, classical FISR lacks fully model-consistent training, limiting predictive accuracy. This study proposes a physics-constrained, multi-objective computational fluid dynamics (CFD)-driven training framework that integrates a CFD solver into gene expression programming for model-consistent training. Correction domains of symbolic expressions are constrained using inversion fields to improve interpretability. The framework is applied to a supersonic compression corner flow using the shear-stress transport (SST) model, yielding the SST-MO model. After appropriate analysis and modification, SST-MO is evaluated on a range of shock-wave/turbulent boundary-layer interaction flows across various Mach numbers, as well as a flat-plate boundary layer to assess its behavior in zero pressure gradient conditions. Classical FISR and single-objective CFD-driven methods are also tested for comparison. Results show that the proposed framework produces a correction model that balances interpretability and predictive performance. Compared to FISR, SST-MO offers improved accuracy, and it maintains greater interpretability than single-objective approaches. The results highlight the potential of multi-objective, physics-informed training for developing practical turbulence model corrections.
KW - Field inversion
KW - Gene expression programming
KW - Model-consistent training
KW - SWTBLI
KW - Turbulence model
UR - https://www.scopus.com/pages/publications/105013239337
U2 - 10.1016/j.ast.2025.110750
DO - 10.1016/j.ast.2025.110750
M3 - 文章
AN - SCOPUS:105013239337
SN - 1270-9638
VL - 168
JO - Aerospace Science and Technology
JF - Aerospace Science and Technology
M1 - 110750
ER -