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Open Access

A novel overset grid strategy and high-order inter-grid boundaries treatment with the cell-centered finite difference method

Xuejun DINGa,bFei LIAOa,b( )Yao JINcJinsheng CAIa,b
School of Aeronautics, Northwestern Polytechnical University, Xi’an 710072, China
National Key Laboratory of Aircraft Configuration Design, Xi’an 710072, China
School of Building Services Science and Engineering, Xi’an University of Architecture and Technology, Xi’an 710055, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

This paper presents an efficient and automated Overset Grid Assembly (OGA) method for the structured grid, and investigates high-order interpolation methods for inter-grid boundaries with the cell-centered finite difference method. Four enhancements are introduced: a hybrid hole-cutting approach integrates the efficiency of approximate hole-cutting and the accuracy and robustness of direct-cutting, effectively addressing challenges such as small gaps and thin cuts; an improved implicit hole boundary optimization method, incorporating quality comparison, can significantly reduce donor search workloads; an improved implicit interpolation cell cancellation algorithm minimizes overlap regions, particularly beneficial for high-order interpolation with large stencils; an algorithm for identifying and eliminating islands without using wall distances, effectively removes islands. The OGA results of a multi-element airfoil, a circular array of cylinders, multiple spheres, and a wing-pylon-store configuration indicate that the proposed method would be a suitable selection for multi-body problems, even in the presence of small gaps and thin geometries. Additionally, for high-order interpolation at inter-grid boundaries, this study presents an optimized interpolation method designed to minimize spectral property errors. Numerical results indicate that for periodic problems frequently crossing inter-grid boundaries, the optimized interpolation is more accurate than classical Lagrange interpolation and would be a suitable selection.

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Chinese Journal of Aeronautics

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Cite this article:
DING X, LIAO F, JIN Y, et al. A novel overset grid strategy and high-order inter-grid boundaries treatment with the cell-centered finite difference method. Chinese Journal of Aeronautics, 2026, 39(3). https://doi.org/10.1016/j.cja.2025.103806

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Received: 01 January 2025
Revised: 15 April 2025
Accepted: 06 June 2025
Published: 06 September 2025
© 2025 The Author(s). Chinese Society of Aeronautics and Astronautics.

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