Numerical Simulation of Melt-wave in Electromagnetic Launcher

Authors

  • Kefeng Yang Air Defense and Antimissile School Air Force Engineering University, Xi’an 710051, China https://orcid.org/0009-0007-4498-9892
  • Gang Feng Air Defense and Antimissile School Air Force Engineering University, Xi’an 710051, China
  • Shaowei Liu Air Defense and Antimissile School Air Force Engineering University, Xi’an 710051, China
  • Xiaoquan Lu Air Defense and Antimissile School Air Force Engineering University, Xi’an 710051, China
  • Xiangyu Du Air Defense and Antimissile School Air Force Engineering University, Xi’an 710051, China
  • Tianyou Zheng Air Defense and Antimissile School Air Force Engineering University, Xi’an 710051, China

DOI:

https://doi.org/10.13052/2024.ACES.J.400807

Keywords:

Electromagnetic launcher, erosion depth, melt-wave, transition, velocity skinning effect

Abstract

To accurately characterize the erosion phenomenon of the armature in electromagnetic railgun launches, a two-dimensional magneto-thermal-mechanical coupling model for melt-wave was developed. For the first time, a fully implicit finite volume method was employed for equation discretization, and an alternating direction implicit method was used for coupling calculations to obtain both steady-state and transient erosion characteristics of the armature. The results demonstrate that the velocity skin effect concentrates significant current at the armature tail, driving the propagation of the melt-wave. The erosion rate remains constant initially but increases significantly when variations in electrical conductivity are considered. After applying an external current, the erosion distance increases sharply with current amplitude before leveling off, and changes in the duration of current amplitude also significantly influence the erosion distance. This study provides a clear understanding of the armature’s erosion behavior, offering a solid theoretical foundation for further research on armature transition phenomenon.

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Author Biographies

Kefeng Yang, Air Defense and Antimissile School Air Force Engineering University, Xi’an 710051, China

Kefeng Yang received the B.S. degree in weapons launch engineering from Air Force Engineering University, Xi’an, China, in 2023. He is currently a graduate student in mechanics at Air Force Engineering University, where his interests include theory and technology of weapon systems, especially about the electromagnetic launch technology.

Gang Feng, Air Defense and Antimissile School Air Force Engineering University, Xi’an 710051, China

Gang Feng received the M.S. degree in weapons from Air Force Engineering University, Xi’an, China. He is currently a Professor at the Air and Missile Defense College, Air

Shaowei Liu, Air Defense and Antimissile School Air Force Engineering University, Xi’an 710051, China

Shaowei Liu received the B.S. and Ph.D. degrees in weapons from the Air Force Engineering University, Xi’an, China, in 2005 and 2008, respectively. He is currently an Associate Professor at the Air Defense and Anti-Missile School, Air Force Engineering University. His current research interests include the theory and technology of weapon systems.

Xiaoquan Lu, Air Defense and Antimissile School Air Force Engineering University, Xi’an 710051, China

Xiaoquan Lu received the B.S. degree in weapons launch engineering from Air Force Engineering University, Xi’an, China, in 2022. He is currently a graduate student in mechanics at Air Force Engineering University, where his interests include theory and technology of weapon systems.

Xiangyu Du, Air Defense and Antimissile School Air Force Engineering University, Xi’an 710051, China

Xiangyu Du received the B.S. degree in weapons in 2020 and the M.S. degree in mechanics in 2023 from the Air Force Engineering University, Xi’an, China, where he is currently pursuing the Ph.D. degree in weapons. His current research interests include theory and technology of weapon systems, especially about electromagnetic launch technology.

Tianyou Zheng, Air Defense and Antimissile School Air Force Engineering University, Xi’an 710051, China

Tianyou Zheng received the B.S. degree in weapons launch engineering from Air Force Engineering University, Xi’an, China, in 2023. He is currently a graduate student in mechanics at Air Force Engineering University, where his interests include contact characteristics of railguns under pulsed high current conditions.

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Published

2025-08-30

How to Cite

[1]
K. . Yang, G. . Feng, S. . Liu, X. . Lu, X. . Du, and T. . Zheng, “Numerical Simulation of Melt-wave in Electromagnetic Launcher”, ACES Journal, vol. 40, no. 08, pp. 745–754, Aug. 2025.

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Section

Advanced Computation with High Performance Computing for Mechanics of Materials

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