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Research Article | Publishing Language: Chinese | Open Access

A curvature-corrected immersion boundary method for adaptive Cartesian meshes

Shangzhi Sun1,2Canyan Luo3Bofu Wang1He Gao2( )Lin Bi2
Shanghai Institute of Applied Mathematics and Mechanics, School of Mechanics and Engineering Sciences, Shanghai University, Shanghai 200072, China
Computational Aerodynamics Institute of China Aerodynamics Research and Development Center, Mianyang 621000, China
College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China
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Abstract

In Cartesian grid methods, the non-body-fitted nature between orthogonal grids and complex solid boundaries poses a significant challenge for accurately imposing boundary conditions, which directly impacts simulation accuracy. The proposed method addresses this by locating reference points along the outward normal direction of the boundary surface, applying bilinear interpolation to obtain the flow variables at those points, and incorporating local curvature information to extrapolate physical quantities. This approach enables accurate reconstruction of flow variables in virtual cells near the boundary, particularly enhancing accuracy in regions with high curvature. Validation on multiple benchmark cases demonstrates a substantial reduction in boundary-induced errors, with errors in the L1, L2 and L norms decreasing by approximately an order of magnitude. The overall method retains second-order convergence and effectively suppresses spurious entropy generation in regions of high curvature, offering a reliable and efficient boundary treatment for Cartesian-grid CFD simulations of complex geometries.

CLC number: O241.82;‌V211.3 Document code: A Article ID: 0258-1825(2026)07-0031-10

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Acta Aerodynamica Sinica
Pages 31-40

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Cite this article:
Sun S, Luo C, Wang B, et al. A curvature-corrected immersion boundary method for adaptive Cartesian meshes. Acta Aerodynamica Sinica, 2026, 44(7): 31-40. https://doi.org/10.7638/kqdlxxb-2025.0055

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Received: 08 March 2025
Revised: 05 May 2025
Published: 03 September 2025
© The journal of Acta Aerodynamica Sinica.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).