通气超空泡稳定性机理与调控研究进展

王志英; 王静竹; 黄荐; 王展; 王一伟

doi:10.6052/1000-0992-24-024

通气超空泡稳定性机理与调控研究进展

doi: 10.6052/1000-0992-24-024 cstr: 32046.14.1000-0992-24-024

王志英¹,
王静竹^{1, 3},
黄荐^{1, 3},
王展^{1, 2},
王一伟^{1, 2, ,}

1.
中国科学院力学研究所流固耦合系统力学重点实验室, 北京 100190
2.
中国科学院大学工学院, 北京 100190
3.
广东空天科技研究院, 广州 511458

基金项目: 国家自然科学基金 (No. 12372243, No. 12122214, No.1229300, No.12293003, No.12293004) 资助项目.

详细信息

作者简介:
王一伟, 中国科学院力学研究所研究员、博士生导师, 主要从事跨介质高速水动力学应用基础问题研究. 已主持173重点项目、国家自然基金优青项目和重大项目课题等任务, 成果应用于重大工程型号研制与新概念装备探索. 目前担任科技部“深海极地装备”重点研发计划专项总体专家组成员、力学学会流体力学专业委员会秘书长、《力学学报》编委、《Journal of Hydrodynamics》执行编委、《水动力学研究与进展》副主编等职, 曾获中国力学学会青年科技奖、科技进步一等奖, 钱学森杰出青年奖、周培源水动力学青年奖等奖项

通讯作者:
wangyw@imech.ac.cn

中图分类号: O352
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- 文章访问数: 55
- HTML全文浏览量: 10
- PDF下载量: 12
- 被引次数: 0
出版历程
- 录用日期: 2024-10-31
- 网络出版日期: 2024-11-16

Research progress on the stability mechanism and control of ventilated supercavitation

WANG Zhiying¹,
WANG Jingzhu^{1, 3},
HUANG Jian^{1, 3},
WANG Zhan^{1, 2},
WANG Yiwei^{1, 2
, ,}

1.
Key Laboratory Mechanics in Fluid Solid Coupling Systems, Institute of Mechanics, Chinese Academy of Sciences, Beijing 100190, China
2.
School of Engineering Science, University of Chinese Academy of Sciences, Beijing 100049, China
3.
Guangdong Aerospace Research Academy, Guangzhou 511458, China

More Information

Corresponding author: wangyw@imech.ac.cn

摘要

摘要: 通气超空泡减阻是突破传统水下速度极限, 实现高速航行的关键技术, 具有重要的工程应用价值. 超空泡航行体的航行稳定性是制约其发展的瓶颈问题, 这与通气超空泡形态的稳定性密切相关, 因此, 超空泡形态的准确预测和调控是超空泡航行体总体设计的关键之一. 本文首先介绍了关于不同环境条件下通气超空泡流动形态特征的研究, 进一步梳理了影响流动形态的关键科学问题, 包括超空泡界面特征及失稳机制、超空泡尾部闭合泄气机理和射流与空泡的耦合作用, 最后基于对通气超空泡形态的理解与认识, 阐述了实现通气超空泡流动稳定性的调控方法.
- 通气超空泡 /
- 泄气机理 /
- 界面失稳机制 /
- 稳定性调控
Abstract: Ventilated supercavity drag reduction is a key technology to break through the traditional underwater speed limit and achieve high-speed operation of underwater vehicles, which has important engineering application value. The navigation stability of underwater vehicles is a bottleneck problem that restricts the development of supercavitating vehicles, which is closely related to the stability of ventilated supercavity. Therefore, accurate prediction and control of supercavity shape are one of the key factors in the overall design of supercavitating vehicles. This paper first introduces the research progress on the flow morphology characteristics of ventilated supercavities under different flow conditions, and further sorts out the key scientific issues that affect the flow morphology, including the characteristics and stability mechanism of the cavity interface, the closure mechanism of the supercavity, and the interaction between the jet and the supercavity. Finally, based on the understanding and recognition of the morphology of ventilated supercavities, a method for achieving flow control of ventilated supercavities is introduced.
- Ventilated supercavity /
- Gas leakage mechanism /
- Cavity interface instability mechanism /
- Regulation of stability

HTML全文

图 1 通气超空泡的航行体的应用

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图 2 通气超空泡结构特征示意图

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图 3 通气空泡典型形态图 (王志英 2018)

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图 4 超空泡形态示意图

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图 5 不同空化水洞中通气空泡形态尺寸对比 (Shao et al. 2017)

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图 6 不同来流阵风频率下通气空泡形态特征 (Lee et al. 2013)

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图 7 近自由面航行空泡形态特征 (Wang 2017)

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图 8 超空泡界面形态特征(Brennen 1970)

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图 9 通气超空泡流动形态特征 (Shao et al. 2018)

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图 10 通气超空泡界面处流动特征 (Jiang et al. 2018)

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图 11 RT和KH组合不稳定性下出现的不稳定模态图谱 (Vadivukkarasan & Panchagnula 2017)

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图 12 不同Fr下通气空泡上界面K-H和R-T不稳定性主导机制转变的临界速度值(Yang et al. 2022)

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图 13 典型泄气方式示意图 (Semenenko & Vladimir 2001)

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图 14 通气超空泡闭合方式图谱 (Karn 等2016)

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图 15 空泡内部气体流动示意图 (Savchenko Y N和Savchenko G Y 2011)

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图 16 通气超空泡剪切层及其内部流动特征 (Wu et al. 2019)

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图 17 通气超空泡界面流动及流场结构特征 (王志英 2018)

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图 18 空化流动中空泡团脱落机制

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图 19 通气空泡团脱落特性 (王志英 2018)

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图 20 通气空泡尾部湍流气泡特征图像 (Barbaca et al. 2019)

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图 21 通气空泡尾迹湍流区气泡流分布特征 (Wang 等2021)

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图 22 不同无量纲参数下射流与空泡闭合耦合作用形态特征划分 (Money et al. 2015)

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图 23 射流作用下通气超空泡泄气模式示意图 (Kinzel et al. 2017)

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图 24 射流作用下通气空泡形态 (周后村 2019)

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图 25 通气闭环控制方案示意图 (辛万青等 2021)

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