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多旋翼近水面效应气动特性实验研究

王宇1,白兴之1,张代贤1,林泽铖1,范召林2,吴文华1   

  1. 1. 跨域飞行交叉技术实验室
    2. 中国空气动力研究与发展中心
  • 收稿日期:2025-05-13 修回日期:2025-07-15 出版日期:2025-07-18 发布日期:2025-07-18
  • 通讯作者: 吴文华
  • 基金资助:
    跨域飞行交叉技术实验室项目(2023-ZY0302)

Experimental Research on the Aerodynamic Characteristics of Near Water Effect of Multi-rotor

  • Received:2025-05-13 Revised:2025-07-15 Online:2025-07-18 Published:2025-07-18
  • Supported by:
    the Key Laboratory of Cross-Domain Flight Interdisciplinary Technology

摘要: 跨介质飞行器的旋翼接近水面时,其下洗气流与水面相互作用会产生复杂的水气交混流场,旋翼在该流场中表现出与地面效应截然不同的气动特性,该现象被称为旋翼近水面效应。相较于单旋翼近水面效应,多旋翼在旋翼间的气动干扰以及各自诱导的水气交混流场的耦合作用下,其近水面效应将变得更加复杂。针对多旋翼近水面效应影响规律和影响因素尚未明晰的研究现状,本文开展了多旋翼近水面气动特性影响实验,对多旋翼近水面条件下不同桨尖间距与旋翼悬停高度下的气动力和转速进行了测量。并结合多旋翼近地面尾迹结构的相关研究与观察到的水气交混流场形态,初步建立了“合并、接触、分离”的多旋翼近水面效应认知框架。在不同水气交混流场状态下,间距最近的合并状态下具有最好的气动性能。随着间距增大,离水面相对较远的接触状态下旋翼无明显拉力损失,而在离水面较近的接触状态下旋翼拉力系数显著降低。此外,桨尖间距最远的分离状态下旋翼与水面作用产生的液滴与旋翼的强交互作用会导致旋翼扭矩剧增。

关键词: 跨介质飞行器, 多旋翼, 近水面效应, 液滴, 水气交混流场, 喷泉效应

Abstract: When the cross-media rotorcrafts approach the water surface, the interaction between its downwash flow and the water surface generates mixed air-water flows. In this flow field, the rotor exhibits aerodynamic characteristics distinctly different from in-ground effect, a phenomenon known as the near-water effect. Compared to the near-water effect of single-rotor, the near-water effect of multi-rotor becomes more complex due to the aerodynamic interference between rotors and the coupling of their respective induced mixed air-water flows. Given the current lack of understanding of the near-water effect of multi-rotor, this paper conducts experiments to investigate the aerodynamic characteristics of multi-rotors near the water surface, measuring the aerodynamic forces and rotational speeds under different blade tip clearances and hovering heights. Combining existing research on the near-ground wake structure of multi-rotors and the observed morphology of the mixed air-water flows, a preliminary cognitive framework of the near-water effect of multi-rotor is established, categorized as "merging, contacting and separating." Under different mixed air-water flows conditions, the merging mode with the closest clearance exhibits the best aerodynamic performance. As the clearance increases, the contacting mode at a relatively higher distance from the water surface shows no significant thrust loss, whereas the contacting mode closer to the water surface results in a notable reduction in the rotor thrust coefficient. Additionally, in the separating mode with the largest blade tip clearance, the strong interaction between the water droplets generated by the rotor-water interaction and the rotor leads to a sharp increase in rotor torque.

Key words: cross-medium vehicle, multi-rotor, near-water effect, droplets, mixed air-water flows, fountain effect

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