| 注册
首页|期刊导航|中国舰船研究|NACA 0012摆动水翼水动力特性的二维数值模拟

NACA 0012摆动水翼水动力特性的二维数值模拟

吕元博 田新亮 李欣 宋春辉

中国舰船研究2018,Vol.13Issue(2):7-15,9.
中国舰船研究2018,Vol.13Issue(2):7-15,9.DOI:10.3969/j.issn.1673-3185.2018.02.002

NACA 0012摆动水翼水动力特性的二维数值模拟

Two-dimensional numerical simulation of NACA 0012 flapping foil hydrodynamics

吕元博 1田新亮 2李欣 1宋春辉2

作者信息

  • 1. 上海交通大学海洋工程国家重点实验室,上海200240
  • 2. 高新船舶与深海开发装备协同创新中心,上海200240
  • 折叠

摘要

Abstract

[Objectives]In order to study the impact of the hydrodynamic performance of foil in the design of a wave glider,[Methods]on account of the characteristics of the oscillating foil when the wave glider is heaving,and based on the Dynamic Fluid Body Interaction(DFBI)module in STAR-CCM+with the SST k-ω turbulence model,the passive oscillating process of foil when it is forced to heave is simulated.The effects of limit angles,wave heights and frequencies on the thrust coefficient of NACA 0012 flapping foil are investigated.[Results]We find that the passive rotation method can effectively simulate foil oscillating process,and its thrust coefficient is about 30% smaller than the coefficient obtained by the active rotation method. Moreover,the maximum limit angle of a wave glider of around 20° gives a better hydrodynamic performance. The numerical simulation result indicate that the thrust coefficient increases with the increase of wave height and wave frequency in a certain region.[Conclusions]This can provide a reference for propulsive performance and hydrodynamic performance under different states of the sea.

关键词

波浪滑翔机/被动摆动/限位角/推进性能

Key words

wave glider/passive oscillating/limit angle/propulsive performance

分类

交通工程

引用本文复制引用

吕元博,田新亮,李欣,宋春辉..NACA 0012摆动水翼水动力特性的二维数值模拟[J].中国舰船研究,2018,13(2):7-15,9.

基金项目

国家自然科学基金资助项目(51509152,11632011) (51509152,11632011)

中国舰船研究

OA北大核心CSCDCSTPCD

1673-3185

访问量0
|
下载量0
段落导航相关论文