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Publishing Language: Chinese | Open Access

Effect of head cone angle on flow field variation during high-speed projectile water entry

Teng LI, Guishan GAO, Weiguang YAO, Yang QIU, Shunzhi HU, Yulin GUI, Yu HE, Xiaobo ZHENG( )
Institute of Fluid Physics, China Academy of Engineering Physics, Mianyang 621999, Sichuan, China
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Abstract

During the high-speed water entry of a projectile, cavitation occurs, forming a cavity bubble that alters the flow field and subsequently affects the projectile’s motion stability. Our study investigates the characteristics of flow field changes after double-cone projectiles with different head cone angles traverse the free surface. High-speed water entry experiments were conducted by using an electromagnetic launch device, and a numerical simulation model of high-speed water entry was established basing on the overset mesh technique and the volume-of-fluid multiphase flow model. The validity of the simulation model was verified through experiments, and the flow field characteristics after the vertical water entry of projectiles with different head types were obtained. The research findings are as follows: After the vertical water entry of a double-cone projectile, the cavity bubble develops symmetrically. Following surface closure of the cavity bubble, its total length increases while its maximum width gradually decreases. As the head cone angle of the projectile's cavitator increases: during the initial entry phase, the closure point and wetted surface position move closer to the tail; the cavity contour becomes wider; the resistance experienced at the moment of entry and during underwater motion increases, leading to faster velocity decay; the time of surface closure for the cavity bubble is delayed. At the same moment during underwater motion, the longer the length of the tail cavity bubble, the shorter the length of the vortex structures within the water domain.

CLC number: O352 Document code: A

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Cite this article:
LI T, GAO G, YAO W, et al. Effect of head cone angle on flow field variation during high-speed projectile water entry. Explosion and Shock Waves, 2026, 46(11). https://doi.org/10.11883/bzycj-2025-0312

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Received: 28 September 2025
Revised: 13 November 2025
Published: 05 November 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/)