Numerical simulation of wake evolution of a propeller with notched blades

被引:6
|
作者
Wu, Tiecheng [1 ,2 ]
Wang, Zhengren [1 ,2 ]
Wang, Lianzhou [3 ]
Cao, Weitao [1 ,2 ]
Luo, Fuqiang [1 ,2 ]
Deng, Rui [1 ,2 ]
机构
[1] Sun Yat Sen Univ, Sch Ocean Engn & Technol, Zhuhai 519082, Peoples R China
[2] Southern Marine Sci & Engn Guangdong Lab Zhuhai, Zhuhai 519082, Peoples R China
[3] Southwest Jiaotong Univ, Sch Mech & Aerosp Engn, Chengdu 611756, Peoples R China
基金
中国国家自然科学基金;
关键词
VORTEX DYNAMICS; MECHANISMS;
D O I
10.1063/5.0222223
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
This study employs an improved delayed detached eddy simulation method to examine the open-water performance and wake evolution of a propeller with notched blades, using an unstructured grid with 52.5 x10(6) cells. The numerical method's validity was confirmed by comparing computed thrust and torque coefficients, as well as the flow field, with experimental data. The findings reveal that notched blades significantly reduce the propeller's hydrodynamic performance and accelerate wake instability. The notches introduce substantial disturbances in the surrounding flow, generating numerous small-scale vortices. These vortices interact with neighboring tip vortices, altering their topology and leading to rapid disintegration and the formation of secondary vortex structures. Increasing the number of notches further destabilizes the tip vortex system, causing tip vortices to lose coherence and become uniformly distributed in the mid-field. This study offers a detailed analysis of how notched blade configurations impact propeller performance, near-field flow characteristics, and wake evolution, providing valuable insights into the underlying mechanisms.
引用
收藏
页数:28
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