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Publishing Language: Chinese

Research status and prospect of cross-media vehicle water exit

Xiongliang YAO1,2, Bin ZHAO1,2, Guihui MA1,2( )
College of Ship Building Engineering, Harbin Engineering University, Harbin 150001, China
Innovation Center for Complex Dynamics and Control, Harbin 150001, China
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Abstract

Cross-media vehicles have become a research hotspot in the field of aerospace-ship interaction because of their high concealment, strong maneuverability and fast penetration by switching between water and air working modes. Sea-air medium crossing involves multiphase flow mixing, unsteady evolution of cavitation and harsh load environment, which threaten the motion stability, water attitude and structural strength of vehicles. Aiming at problems of evolution characteristics of the shoulder/exhaust cavity flow and the tail cavity, and the collapse and load characteristics of the cross water-air medium during the cross-medium water exit process of the vehicle, this paper expounds the research status of the mechanism of the shoulder/tail cavity flow during the underwater navigation and water exit process of the cross-medium vehicle in the aerospace-ship crossover field in recent years. The research on the collapse and load characteristics of the cross sea-air medium process is summarized, and the cross domain water exit problems involving different launch environments are listed. Finally, the problems to be solved and the future development trend in the field of aerospace-ship crossover are summarized and discussed.

Keywords

cross-media vehiclewater exitcavity shapehydrodynamic characteristicsventilatory
CLC number: V211; TJ6 Document code: A

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Acta Aeronautica et Astronautica Sinica
Volume 45 Issue 14,
July 2024
Article number: 029598
DOI: 10.7527/S1000-6893.2023.29598
Cite this article:
YAO X, ZHAO B, MA G. Research status and prospect of cross-media vehicle water exit. Acta Aeronautica et Astronautica Sinica, 2024, 45(14): 029598. https://doi.org/10.7527/S1000-6893.2023.29598

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Received: 18 September 2023
Revised: 13 October 2023
Accepted: 08 November 2023
Published: 17 November 2023
© 2024 The Journal of Acta Aeronautica et Astronautica Sinica
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