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巡航状态下泵喷推进潜艇尾部喷流涡特性研究

郭荣 王乾年 韩伟 李舟睿

华中科技大学学报(自然科学版)2024,Vol.52Issue(4):94-99,6.
华中科技大学学报(自然科学版)2024,Vol.52Issue(4):94-99,6.DOI:10.13245/j.hust.240065

巡航状态下泵喷推进潜艇尾部喷流涡特性研究

Study on characteristics of pump-jet propelled submarine tail jet vortex under cruising conditions

郭荣 1王乾年 2韩伟 1李舟睿2

作者信息

  • 1. 兰州理工大学能源与动力工程学院,甘肃 兰州 730050||甘肃省流体机械及系统重点实验室,甘肃 兰州 730050
  • 2. 兰州理工大学能源与动力工程学院,甘肃 兰州 730050
  • 折叠

摘要

Abstract

The detached eddy simulation(DES)model was used to simulate the pump-boat model under cruising conditions.Ω criterion was used to identify and capture the vortex structure in the flow field of the pump jet tail at different speeds,and the dynamic characteristics of the jet vortex were studied.Results show that the external flow around the submarine and the pump-jet propeller could interact with the tail flow,resulting in different flow field regions.With the increase of speed,the irrotational zone and the range of flow field diffusion zone increase,the body flow around the jet and the tail flow produce strong coupling effect at a faster speed,and develop and move along the opposite direction of the submarine.The range and energy of shear layer vortexes and the energy of shedding vortexes also increase with the speed increasing.During the rotation period,the hub vortex and the shedding vortex in the middle of the flow field have weak mutual influence,and the two vortices rotate irregularly along the rotating direction of the impeller,while the two vortices at the tail of the flow field produce complex influences and produce irregular changes and movements with time.

关键词

泵喷推进器/巡航状态/尾部喷流/涡特性/Ω准则

Key words

pump-jet propulsion/cruising conditions/tail jet/vortex characteristic/Ω criterion

分类

交通工程

引用本文复制引用

郭荣,王乾年,韩伟,李舟睿..巡航状态下泵喷推进潜艇尾部喷流涡特性研究[J].华中科技大学学报(自然科学版),2024,52(4):94-99,6.

基金项目

国家自然科学基金资助项目(52009050) (52009050)

中国博士后科学基金资助项目(2020M673537) (2020M673537)

甘肃省自然科学基金资助项目(20JR10RA172) (20JR10RA172)

兰州理工大学红柳优秀青年人才支持计划项目. ()

华中科技大学学报(自然科学版)

OA北大核心CSTPCD

1671-4512

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