基于南海波浪要素的波浪滑翔机翼板参数优化设计与仿真

doi:10.11978/2020054

热带海洋学报 ›› 2021, Vol. 40 ›› Issue (2): 112-119.doi: 10.11978/2020054CSTR: 32234.14.2020054

基于南海波浪要素的波浪滑翔机翼板参数优化设计与仿真

吴世其(), 洪梅(), 陈希, 毛科峰, 刘科峰

国防科技大学气象海洋学院, 江苏南京 211101

收稿日期:2020-05-23 修回日期:2020-08-29 出版日期:2021-03-10 发布日期:2020-09-12
通讯作者: 洪梅
作者简介:吴世其(1996—), 男, 江苏省苏州市人, 硕士研究生, 主要从事海洋调查研究。email: wushiqi17@nudt.edu.cn
基金资助:
国家自然科学基金面上项目(41875061);国家自然科学基金面上项目(41075045);国家自然科学基金面上项目(41775165);国家自然科学基金面上项目(51609254);江苏省自然科学基金面上项目(BK20161464);湖南省自然科学基金(2020JJ4661);国防科技大学校内科研项目(ZK18-03-48)

Design of Wave Glider optimal wing parameters suitable for the South China Sea

WU Shiqi(), HONG Mei(), CHEN Xi, MAO Kefeng, LIU Kefeng

College of Meteorology and Oceanography, National University of Defense Technology, Nanjing 211101, China

Received:2020-05-23 Revised:2020-08-29 Online:2021-03-10 Published:2020-09-12
Contact: HONG Mei
Supported by:
National Nature Science Foundation of China(41875061);National Nature Science Foundation of China(41075045);National Nature Science Foundation of China(41775165);National Nature Science Foundation of China(51609254);Nature Science Foundation of Jiangsu(BK20161464);Nature Science Foundation of Hunan(2020JJ4661);National University of Defense Technology(ZK18-03-48)

摘要/Abstract

摘要：

针对南海不同波浪要素条件下波浪滑翔机翼板参数设计的问题进行研究。基于欧洲中尺度天气预报中心大气和海洋全球再分析数据集(ERA5), 对南海不同季节以及台风经过时的波高波周期进行统计。并利用FLUENT软件研究南海不同波浪要素条件下翼板最大偏转角度、转轴位置以及翼板间距对波浪滑翔机水下翼板平均推力的影响。仿真结果表明, 波高越大, 翼板最大偏转角度也应相应增大, 才能保证翼板获得更大的推力; 在南海波浪要素条件下, 翼板转轴位置选取在翼板前端1/5处较佳; 适当增加翼板间距能够提高翼板获得的推力。通过对翼板被动摆动进行仿真, 得到了翼板在不同参数设置下产生的推力, 为波浪滑翔机翼板设计提供参考。

关键词: 波浪滑翔机, 最大偏转角度, 转轴位置, 翼板间距

Abstract:

In view of different wave height and period in the South China Sea, the design of Wave Glider wing parameters is studied to obtain greater thrust. Based on the reanalysis data set of ERA5, we provide statistics on the wave height and wave period of different seasons and induced by one typhoon in the South China Sea. In addition, the software FLUENT is used to study the influence of the maximum limit angle, the position of rotating axis and the spacing of the wings. The simulation results show that the larger the wave height, the larger the maximum limit angle should be in order to ensure that the wings can get more thrust. Under the conditions of wave height and period in the South China Sea, it is better to select 1/5 of the front of the wing as the position of rotating axis. Increasing the spacing of the wings properly can improve the thrust. By simulating the flapping wings, the thrust generated by the wings under different parameters is obtained, which provides a reference for the design of the wings.

Key words: Wave Glider, maximum limit angle, position of rotating axis, spacing of the wings

中图分类号:

P716.1

吴世其, 洪梅, 陈希, 毛科峰, 刘科峰. 基于南海波浪要素的波浪滑翔机翼板参数优化设计与仿真[J]. 热带海洋学报, 2021, 40(2): 112-119.

WU Shiqi, HONG Mei, CHEN Xi, MAO Kefeng, LIU Kefeng. Design of Wave Glider optimal wing parameters suitable for the South China Sea[J]. Journal of Tropical Oceanography, 2021, 40(2): 112-119.

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	波高/m	波周期/s
春季	0.96	5.39
夏季	1.04	5.21
秋季	1.44	6.32
冬季	1.79	6.50
全年	1.31	5.85
台风风眼附近	5.15	8.61

网格编号	总网格数/个	背景网格数量/个	重叠网格数量/个	平均推力/N
A1	49630	21280	28350	40.3
A2	79053	33400	45653	42.7
A3	114788	48000	66788	43.5
A4	152815	68068	84747	43.5

基于南海波浪要素的波浪滑翔机翼板参数优化设计与仿真

Design of Wave Glider optimal wing parameters suitable for the South China Sea

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