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Open Access

A multi-body separation simulation method incorporating a high-efficiency and high-precision collision model

Jiaxuan YEaWei TIANaShuling TIANb( )Yunfei MIAOaJiaming ZHANGaJinjun DUANa
College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

Multi-body separation involving collisions is common in aerospace engineering. The ability to analyze the dynamics of multi-body collisions is rarely possessed by traditional Multi-Body Separation Simulation (MBSS) methods. To methodically address this challenging issue, a research study is conducted herein based on the MBSS in conjunction with an efficient and high-accuracy collision model. First, an MBSS based on the dynamic unstructured overset grid method is performed by solving the unsteady compressible Reynolds-averaged Navier-Stokes equations with the six-degree-of-freedom rigid-body motion. Second, to detect object collisions and calculate collision factors with high accuracy and efficiency, a collision detection approach and a nearest distance calculation based methodology on the basis of computational fluid dynamics data structures and bounding volume hierarchies are originally proposed. Third, a transient multiple collision model is established to simulate an unlimited number of object collisions within a single time step. Finally, collision simulation experiments with balls and those of the space shuttle’s collision with foreign objects are conducted to verify the accuracy, efficiency, and robustness of the newly developed approach.

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Chinese Journal of Aeronautics

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Cite this article:
YE J, TIAN W, TIAN S, et al. A multi-body separation simulation method incorporating a high-efficiency and high-precision collision model. Chinese Journal of Aeronautics, 2026, 39(4). https://doi.org/10.1016/j.cja.2025.103777

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Received: 13 February 2025
Revised: 08 April 2025
Accepted: 05 May 2025
Published: 19 August 2025
© 2025 The Author(s). Chinese Society of Aeronautics and Astronautics.

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