Propulsion performance investigation of bio-inspired nano rotor base on fluid–structure interaction

IF 1.5 4区 工程技术 Q2 ENGINEERING, AEROSPACE International Journal of Micro Air Vehicles Pub Date : 2020-01-01 DOI:10.1177/1756829319900886
Shanyong Zhao, Zhen Liu, P. Che, Bingfei Li, Tianjiao Dang, Chen Bu
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Abstract

In this paper, the bio-inspired blade motion is introduced to improve the propulsive performance of nano rotor at an ultra-low Reynolds number. However, the complex flow interacts with the flexible composite blade structure resulting in the change of nano rotor propulsion performance and the vibration of blade structure. A composite nano rotor with blade-pitch motion is investigated computationally with a computational solvers based on fluid–structure interaction. The finite element model for the composite rotor is created and verified with a non-contact modal test. It is found that the simulation results matched well with the experimental results. Successively, the propulsive performance of a rigid nano rotor is studied. The propulsive performance of the nano rotor is analysed at different bio-inspired pitch frequencies. The results show that the figure of merit of the bio-inspired pitch rotor increases because of the bio-inspired blade pitch motion. And it is also found that the improvement of the propulsive performance of the nano rotor varies with the pitch frequency. The propulsive performance of the flexible bio-inspired nano rotor is also studied with by using fluid–structure interaction method. It is found that the computational results for flexible nano rotor are lower than that for rigid nano rotor. It is evident that it is necessary to consider the flexibility of the composite nano rotor when investigating the propulsion performance of bio-inspired nano rotor. And the response of blade structure is also studied. Structural dynamic analysis shows that the blade structure vibrates with small amplitude. And two peak values are found at the rotation frequency and the fundamental frequency of the nano rotor structure.
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基于流固耦合的仿生纳米转子推进性能研究
本文引入生物激励叶片运动来改善纳米转子在超低雷诺数下的推进性能。然而,复杂的流动与柔性复合材料叶片结构相互作用,导致纳米转子推进性能的变化和叶片结构的振动。采用基于流体-结构相互作用的计算求解器,对具有叶片变桨运动的复合材料纳米转子进行了计算研究。建立了复合材料转子的有限元模型,并通过非接触模态试验进行了验证。仿真结果与实验结果吻合良好。接着,对刚性纳米转子的推进性能进行了研究。分析了纳米旋翼在不同生物激励桨距频率下的推进性能。结果表明,生物激励变桨转子的优值随着叶片的变桨运动而增大。研究还发现,纳米旋翼推进性能的改善程度随桨距频率的变化而变化。采用流体-结构相互作用方法研究了柔性仿生纳米转子的推进性能。研究发现,柔性纳米转子的计算结果低于刚性纳米转子。显然,在研究仿生纳米转子的推进性能时,有必要考虑复合材料纳米转子的柔性。并对叶片结构的响应进行了研究。结构动力学分析表明,叶片结构存在小振幅振动。在纳米转子结构的旋转频率和基频处发现了两个峰值。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
CiteScore
3.00
自引率
7.10%
发文量
13
审稿时长
>12 weeks
期刊介绍: The role of the International Journal of Micro Air Vehicles is to provide the scientific and engineering community with a peer-reviewed open access journal dedicated to publishing high-quality technical articles summarizing both fundamental and applied research in the area of micro air vehicles.
期刊最新文献
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