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Simulation analysis on characteristics of flow field induced by submerged supersonic jets
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Xu-gang WANG1, 2, Yue CAO3, Jia XU2, Fan-yu WANG2, Jian-yang YU3
Journal of Ship Mechanics | 2025, 29(7) : 1048 - 1060
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Journal of Ship Mechanics | 2025, 29(7): 1048-1060
Hydrodynamics
Simulation analysis on characteristics of flow field induced by submerged supersonic jets
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Xu-gang WANG1, 2, Yue CAO3, Jia XU2, Fan-yu WANG2, Jian-yang YU3
Affiliations
  • 1.College of Shipbuilding Engineering, Harbin Engineering University, Harbin 150009, China
  • 2.Beijing Institute of Aerospace Systems Engineering, Beijing 100076, China
  • 3.School of Energy Science and Engineering, Harbin Institute of Technology, Harbin 150001, China
Published: 2025-07-20 doi: 10.3969/j.issn.1007-7294.2025.07.004
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This paper investigates the characteristics of the flow field induced by a supersonic jet at the tail of an underwater axisymmetric vehicles under different pressure ratio conditions, based on the volume of fluid (VOF) multiphase flow model. The study analyzes the evolution of the flow field at the tail of the axisymmetric vehicles and explores the morphological distribution of the induced cavity at various time instances under different pressure ratios. The research findings indicate a close relationship between the jet’s tail cavity morphology and the nozzle pressure ratio. When the pressure ratio is relatively low, the tail cavity exhibits a conical shape similar to the supercavitation. As the pressure ratio increases, the influence of the tail vortex on the jet gradually diminishes, and the high-pressure ratio jet evolves into a pulsating jet under the action of shear entrainment driven by the Kelvin-Helmholtz instability. Within the pulsating jet flow field, phenomena such as “back-attack” and pressure disturbances in the water medium lead to a “positive feedback” effect on the pulsation characteristics of the jet. After the high-pressure ratio jet transforms into a pulsating jet, the degree of jet necking fluctuates significantly with time, and the initial bubble breakup results in a random distribution of the jet necking location with time. With a further increase in pressure ratio, the morphology of the pulsating tail cavity tends to stabilize, and the pressure fluctuation amplitude at the bottom of the axisymmetric vehicles decreases.

submerged supersonic gas jet  /  multiphase  /  tail cavity  /  numerical simulation
Xu-gang WANG, Yue CAO, Jia XU, Fan-yu WANG, Jian-yang YU. Simulation analysis on characteristics of flow field induced by submerged supersonic jets[J]. Journal of Ship Mechanics, 2025 , 29 (7) : 1048 -1060 . DOI: 10.3969/j.issn.1007-7294.2025.07.004
Year 2025 volume 29 Issue 7
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Article Info
doi: 10.3969/j.issn.1007-7294.2025.07.004
  • Receive Date:2025-01-17
  • Online Date:2026-03-24
  • Published:2025-07-20
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  • Received:2025-01-17
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Affiliations
    1.College of Shipbuilding Engineering, Harbin Engineering University, Harbin 150009, China
    2.Beijing Institute of Aerospace Systems Engineering, Beijing 100076, China
    3.School of Energy Science and Engineering, Harbin Institute of Technology, Harbin 150001, China
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表12种不同金属材料的力学参数

Family
属数
Number of
genus
种数
Number of
species
占总种数比例
Percentage of
total species (%)

Genus
种数
Number of
species
占总种数比例
Percentage of total
species (%)
鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
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