Abstract

When tire burst debris impacts a wing fuel tank, the momentum and kinetic energy are transferred to the fluid and the surrounding structure, which increases the risk to the aircraft. In this paper, two types of hydrodynamic effects, defined as the pressure wave mode and the fluid displacement mode, were investigated in the process of tire burst debris impacting a wing tank, and an accurate numerical model was established. A fluid–solid interaction (FSI) model with the coupled Eulerian–Lagrangian (CEL) method is proposed to reproduce the hydrodynamic effects; the model fully considers the interaction between the tank and the fuel, and the accuracy of the numerical model was verified by experiments that met the airworthiness conditions. Analysis of the pressure wave propagation, fuel pressure, fuel displacement, and cavity evolution showed that the pressure wave first affects the structure, then the fluid gradually evolves a cavity near the impact point, and finally the fluid displacement significantly increases the impact on the structure. The numerical analysis method for simulating the hydrodynamic effects of tire burst debris impacting a wing tank is presented and was evaluated. It can provide a reference for airworthiness certification and structural design of aircraft.

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Data Availability Statement

Some or all data, models, or code that support the findings of this study are available from the corresponding author upon reasonable request.

Acknowledgments

This work was supported by the Natural Science Foundation of Shaanxi Province (Grant No. S2021-JC-YB-0590). The authors deliver their sincere thanks to the editors and anonymous reviewers.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 37Issue 1January 2024

History

Received: May 4, 2023
Accepted: Sep 18, 2023
Published online: Nov 9, 2023
Published in print: Jan 1, 2024
Discussion open until: Apr 9, 2024

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Chenchen Lian, Ph.D. [email protected]
Ph.D. Student, School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical Univ., Xi’an 710100, China. Email: [email protected]
Pengyu Ye, Ph.D.
Engineer, Shaanxi Qianshan Avionics Co., Ltd., Shaanxi 710065, China.
Associate Professor, School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical Univ., Xi’an 710100, China (corresponding author). ORCID: https://orcid.org/0000-0001-8914-1210. Email: [email protected]
Zhufeng Yue, Ph.D.
Professor, School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical Univ., Xi’an 710100, China.
Haowei Yang, Ph.D.
Ph.D. Student, School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical Univ., Xi’an 710100, China.
Ke Zhang, Ph.D.
Associate Researcher, School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical Univ., Xi’an 710100, China.
Jianmin Zhang, Ph.D.
Engineer, Dept. of Shanghai Aircraft Design and Research Institute, Commercial Aircraft Corporation of China, Ltd., Shanghai 200120, China.

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