Fluid Dynamics of Interacting Rotor Wake with a Water Surface

Author:

Bai Xing-Zhi1,Zhang Zhe12,Wu Wen-Hua1,Wang Xiao3ORCID,Zhan Qi3ORCID,Zhang Dai-Xian1,Yu Lei1

Affiliation:

1. Key Laboratory of Cross-Domain Flight interdisciplinary Technology, China Aerodynamics Research and Development Center, Mianyang 621000, China

2. College of Shipbuilding Engineering, Harbin Engineering University, Harbin 150001, China

3. National Key Laboratory of Helicopter Aeromechanics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

Abstract

Rotor-type cross-media vehicles always induce considerably complex mixed air–water flows when approaching the water surface, resulting in relative thrust loss and structural damage on rotor. The interactions between a water surface and rotor wake bring potential risks to the cross-media process, which is known as the near-water effect of the rotor. In this paper, experimental investigations are used to explore the fluid dynamics of the near-water effect of the rotor. Qualitative droplet observation was carried out on the 0.25 m and 0.56 m diameter commercial rotor blades and the 0.07 m diameter ducted fan near the water surface first to gain a qualitative understanding of droplet characteristics. The results show that the rotor wake caused water surface deformation, droplet tearing off, splashing, and entrainment into the rotor disk. The depression formed by the rotor downwash flow impacting the water surface is named as three modes: dimpling, splashing, and penetrating, and the correlation between the depression modes and the aerodynamic characteristics of the rotor is primary analyzed. The flow mechanisms of dimpling mode were studied using the particle image velocimetry (PIV) technique. The results showed that the cavity and liquid crown obviously alter the flow direction of water surface jets, but not all rotors near water enter the vortex ring state. Two splashing mechanisms were revealed, including the direct ejection of droplets at the rim of depression and the tearing of liquid crown by the water surface jets. The blade tip vortex in the surface jet is a potential cause of entrainment into the rotor disk and secondary breakup of the droplet.

Funder

Key Laboratory of Cross-Domain Flight interdisciplinary Technology

Publisher

MDPI AG

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