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Weiji Wang

Publications and source records attributed to Weiji Wang.

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Manifold Learning with Implicit Physics Embedding for Reduced-Order Flow-Field Modeling

Nonlinear manifold learning (ML) based reduced-order models (ROMs) can substantially improve the quality of nonlinear flow-field modeling. However, noise and the lack of physical information often distort the dimensionality-reduction process, reducing the robustness and accuracy of flow-field prediction. To address this problem, we propose a novel manifold learning ROM with implicit physics embedding (IPE-ML). Starting from data-driven manifold coordinates, we incorporate physical parameters (e.g., angle of attack, Mach number) into manifold coordinates system by minimizing the prediction error of Gaussian process regression (GPR) model, thereby fine-tuning the manifold structure. These adjusted coordinates are then used to construct a flow-fields prediction model that predict nonlinear flow-field more accurately. The method is validated on two test cases: transonic flow-field modeling of the RAE2822 and supersonic flow-field modeling of the hexagon airfoil. The results indicate that the proposed IPE-ML can significantly improve the overall prediction accuracy of nonlinear flow fields. In transonic case, shock-related errors have been notably reduced, while in supersonic case the method can confine errors to small local regions. This study offers a new perspective on embedding physical information into nonlinear ROMs.

physics.flu-dyn

A Kernel Ridge Regression Combining Nonlinear ROMs for Accurate Flow Field Reconstruction with Discontinuities

Nonlinear reduced-order models (ROMs), represented by manifold learning (ML), can effectively improve the modeling accuracy of nonlinear flow fields with discontinuities. However, the inverse mapping from low-dimensional manifold coordinates to high-dimensional flow fields often introduces considerable reconstruction errors, leading to inaccuracy in the locations of discontinuities. To address this challenge, a novel reconstruction method is proposed to enhance the accuracy of reconstructing flow fields with discontinuities. The method employs kernel ridge regression (KRR) to construct a set of nonlinear modes rich in discontinuity information, sequentially these modes are nonlinearly combined with manifold coordinates to achieve accurate flow field reconstruction. The proposed reconstruction method is validated to reconstruct the transonic flow fields over RAE2822 airfoil. Comparison results demonstrate that the method achieves superior reconstruction accuracy compared to existing approaches, especially in reconstructing flow fields' discontinuous regions and precisely capturing discontinuities. This work provides an effective and highly interpretable solution for improving the accuracy of nonlinear ROMs in discontinuous flow fields modeling.

physics.flu-dyn