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The flow field around a rotor in axial descent

Published online by Cambridge University Press:  21 June 2005

RICHARD B. GREEN
Affiliation:
Department of Aerospace Engineering, University of Glasgow, G12 8QQ, UK
ERIC A. GILLIES
Affiliation:
Department of Aerospace Engineering, University of Glasgow, G12 8QQ, UK
RICHARD E. BROWN
Affiliation:
Department of Aeronautics, Imperial College, London, SW7 2AZ, UK

Abstract

Measurements of the flow field around a model rotor descending axially into its own vortex wake have been performed using particle image velocimetry (PIV). At low descent rates, the expected cylindrical down-flow structure below the rotor is observed. At slightly higher descent rate, the flow enters the so-called vortex ring state (VRS) where the vorticity from the rotor accumulates into a toroidal structure near the rotor tips, and a large recirculation zone forms above the rotor disk. In the VRS, the flow below the rotor shows a significant upwards component, with a small up-flow zone penetrating right up to the rotor disk. Measurements show there to be a range of descent rates just before the onset of the VRS over which the flow may be interpreted to be in an incipient VRS condition. In this range, analyses of individual PIV measurements indicate that the flow near the rotor intermittently switches between the down-flow topology found at lower descent rates and the flow topology found in the fully developed VRS. The frequency of excursions of the flow into the VRS topology increases as the descent rate of the rotor is increased until, at high enough descent rate, the flow remains locked within its toroidal state.

Type
Papers
Copyright
© 2005 Cambridge University Press

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