Performance of Semi-Active Flapping Hydrofoil with Arc Trajectory

被引:7
|
作者
Zhou, Junwei [1 ]
Yan, Wenhui [2 ]
Mei, Lei [1 ]
Shi, Weichao [3 ]
机构
[1] Harbin Inst Technol, Sch Ocean Engn, Weihai 264209, Peoples R China
[2] North China Univ Technol, Sch Mech & Mat Engn, 5 Jinyuanzhuang Rd, Beijing 100144, Peoples R China
[3] Strathclyde Univ, Dept Naval Architecture Ocean & Marine Engn, Glasgow City G4 0LZ, Scotland
基金
中国国家自然科学基金;
关键词
flapping foil propulsion; circular arc trajectory; semi-active flapping foil; spring stiffness; performance analysis; OSCILLATING FOILS; PROPULSION;
D O I
10.3390/w15020269
中图分类号
X [环境科学、安全科学];
学科分类号
08 ; 0830 ;
摘要
The semi-active flapping foil driven by the swing arm is a simple structure to realize the propulsion of the flapping foil. The motion trajectory of this semi-active flapping foil mechanism is a circular arc, and its hydrodynamic characteristics are not clear. This paper systematically investigates the working characteristics and hydrodynamic performance of this semi-active flapping foil with a circular arc track. Compared with the traditional flapping foil structure, the special design parameters of the semi-active flapping foil driven by the swing arm mainly include the length of the swing arm and the stiffness of the torsion spring. In this paper, the three-dimensional fluid-structure coupling method is used by solving the fluid dynamics equation and the structural dynamics equation, and the working characteristics of the structure with different motion and geometric parameters are analyzed. From the results, increasing the swing arm length is beneficial to improving the peak efficiency of the flapping foil, and also to improving the thrust coefficient corresponding to the peak efficiency point. Under a certain swing arm length, reducing the spring stiffness is also conducive to improving the peak efficiency of the propulsion system, but it is adverse to the thrust coefficient. Further analysis shows that the maximum angle of attack is the key factor affecting the efficiency of this flapping foil propulsion. For the flapping foil described in this paper, its peak efficiency is usually concentrated near alpha(max) = 0.2 rad. However, for the thrust coefficient of this kind of flapping foil propulsion, the influencing factors are relatively complex, including swinging arm, the spring stiffness, and the advance coefficient. The maximum angle of attack remains the key factor affecting the peak thrust in the range of advance coefficient far from the starting state.
引用
收藏
页数:18
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