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Publishing Language: Chinese | Open Access

Study of the characteristics of fuel spurt caused by high-velocity fragment impact the fuel tank

Anran CHEN1,2Haihua CHEN1Yao YU1Fuguo BIAN3Haojie YU1Xiangdong LI2( )
Shanghai Electro-Mechanical Engineering Institute, Shanghai 201109, China
School of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing 210094, Jiangsu, China
Shanghai Academy of Spaceflight Technology, Shanghai 201109, China
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Abstract

When a high-velocity fragment impacted the fuel tank, hydrodynamic ram occurred. The fuel spurt caused by hydrodynamic ram may result in the ignition or even explosion of the fuel tank, thus threatening the survivability of the high-value target. To study the characteristics of fuel spurt caused by the hydrodynamic ram event, an experiment of a high-velocity fragment impacting a simulated fuel tank was conducted, and the characteristics of velocity and spatial distribution of the fuel spurt were tested and analyzed. In order to quantitatively describe the initial motion velocity of the fuel spurt and the attenuation process of its movement in the air, the specific volume unit within the fuel was defined as fuel mass. The concepts of initial motion velocity v0 and dispersion velocity of the fuel mass were proposed. The process of fuel mass spurting from the penetration orifices was simplified into three stages: (1) the fuel mass was about to spurt out; (2) the fuel mass spurted from the penetration orifices; (3) the fuel mass was moving in the air and gradually became atomized. On this basis, the theoretical model of the distribution of fuel spurt was established. According to the cracks at the penetration orifices and the shape change of the material at the edge of the orifices, the value of the coefficient of discharge was classified, and the influence of the distribution of pressure in the fuel was also taken into account during the calculation. When v0≤737 m/s, the range of Cv is from 0.60 to 0.70. When 737 m/s<v0<906 m/s, Cv ranges from 0.25 to 0.55. When v0≥906 m/s, Cv ranges from 0.75 to 0.95. The research showed that the average error between the calculation results of the fuel spurt axial distance and the experimental results was less than 15%. The error between the calculation results of the corrected theoretical model of radial distance and the experimental results was about 5%. The calculated results of the theoretical model were in good agreement with the experimental results.

CLC number: O358 Document code: A

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Cite this article:
CHEN A, CHEN H, YU Y, et al. Study of the characteristics of fuel spurt caused by high-velocity fragment impact the fuel tank. Explosion and Shock Waves, 2026, 46(6). https://doi.org/10.11883/bzycj-2025-0100

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Received: 27 March 2025
Revised: 19 October 2025
Published: 05 June 2026
© 2026 Editorial Office of Explosion and Shock Waves

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