华南理工大学学报(自然科学版) ›› 2015, Vol. 43 ›› Issue (11): 127-132,144.doi: 10.3969/j.issn.1000-565X.2015.11.018

• 力学 • 上一篇    下一篇

航行器在空中飞行与水下潜航时的动力学特性

杨海燕1,郑姬林1,吝科2   

  1. 1. 陕西师范大学 物理学与信息技术学院,陕西 西安 710061; 2. 空军工程大学 空管领航学院,陕西 西安 710051
  • 收稿日期:2014-10-30 修回日期:2015-06-24 出版日期:2015-11-25 发布日期:2015-10-01
  • 通信作者: 杨海燕(1972-),女,博士,副教授,主要从事航行体设计与仿真研究. E-mail:yanghy07@yeah.net
  • 作者简介:杨海燕(1972-),女,博士,副教授,主要从事航行体设计与仿真研究.
  • 基金资助:
    国家自然科学基金面上项目(61472441)

Investigation into Aerodynamic and Hydrodynamic Characteristics of Trans-Media Vehicle

Yang Hai-yan1  Lin Shu-yu1  Lin Ke2   

  1. 1. College of Physics and Information Technology,Shaanxi Normal University,Xi'an 710061,Shaanxi,China;
    2. College of Air Traffic Control and Navigation,Air Force Engineering University,Xi'an 710051,Shaanxi, China
  • Received:2014-10-30 Revised:2015-06-24 Online:2015-11-25 Published:2015-10-01
  • Contact: 杨海燕(1972-),女,博士,副教授,主要从事航行体设计与仿真研究. E-mail:yanghy07@yeah.net
  • About author:杨海燕(1972-),女,博士,副教授,主要从事航行体设计与仿真研究.
  • Supported by:
     Supported by the National Natural Science Foundation of China(61472441)

摘要: 空气和水两种介质物理性质的巨大差异会对跨介质航行器的动力学环境产生复杂影响. 文中以雷诺数为参考,采用 CFX 软件设计案例进行仿真,研究航行器在跨越不同流体介质时的动力学特性. 仿真结果表明:跨越过程中流场存在一个雷诺数拐点,雷诺数小于拐点时,若水和空气的雷诺数相同,航行器的水、空流体动力学参数随攻角变化的趋势一致且数值相近;若水和空气的雷诺数相似,则存在一个匹配的飞行与潜航速度区间,仍能满足水、空介质间相似的动力学特性. 文中研究结论可为航行器的航行控制提供设计依据.

关键词: 雷诺数, 数值仿真, 气动特性, 水动特性

Abstract: The huge physical-characteristic differences between air and water would produce complicated impact on
the dynamic environment of trans-media vehicles. In this paper,with the Reynolds number (Re) as reference,the dynamic property of the vehicles crossing different fluids are simulated by using the software CFX to design cases. Simulation results show that there exists a Re inflection point in the flow field during the crossing process,and that,when Re is less than the inflection point,if the Re of the air and the Re of the water are the same,the change trends of aerodynamic parameters and hydrodynamic ones with the attack angle are consistent and their numerical values are similar,and if the Re of the air is close to that of the water,there exists a matching range between flight speed and submerged speed,in which the aerodynamic characteristics are shown to be similar to the hydrodynamic ones. The conclusions can provide a basis for the design of voyage control.

Key words: Reynolds number, numerical simulation, aerodynamic characteristics, hydrodynamic characteristics