Abstract

We present results from an experimental investigation of two closely spaced helical vortices. The two co-rotating vortices are generated in a water channel by a one-bladed rotor, whose tip geometry is modified by the addition of a perpendicular fin on the pressure side. The fin parameters are tuned so that the two vortices have approximately equal circulation. Dye visualisations and flow field measurements from Particle Image Velocimetry show that the vortices merge into a single tip vortex within less than one rotor rotation. This fast merging is caused by a rapid increase of the core radii of the initial vortices, which indicates the presence of an instability phenomenon. Analysis of the vortex velocity profiles identifies it as a centrifugal instability, linked to the presence of opposite-signed vorticity in the blade tip region. We further explore the origin of this vorticity by modifying the streamwise fin position. Measurements suggest that the interaction between the secondary fin vortex and the blade surface is partly responsible for the generation of the unstable velocity profile. The vortex resulting from the merging has a significantly larger core size than the one developing without a fin, indicating that this configuration could be beneficial in the context of Blade-Vortex Interaction noise for helicopters, or for the reduction of fatigue loads on wind turbine rotors caused by the interaction with concentrated tip vortices in the wake of upstream turbines.

Highlights

  • Many engineering application involve rotating blades, e.g. horizontal-axis wind turbines, helicopters and marine propellers

  • The flow generated by these rotor configurations is characterised by the existence of interlaced helical vortices emanating from the blade tips, which are a consequence of the lift force responsible for the thrust

  • E↵ect of the fin on tip vortex evolution We here briefly recall the key findings from a previous study presented in [12]

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Summary

Introduction

Many engineering application involve rotating blades, e.g. horizontal-axis wind turbines, helicopters and marine propellers. The values obtained with the experimentally measured profiles are compatible with the observed rapid growth of the initial core size, identifying centrifugal instability as a key element leading to a very fast merging in our configuration.

Results
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