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Measurements of the Early Development of Trailing Vorticity from a RotorThe wake behind a two-bladed model rotor in light climb was measured using particle image velocimetry, with particular emphasis on the development of the trailing vortex during the first revolution of the rotor. The distribution of vorticity was distinguished from the slightly elliptical swirl pattern. Peculiar dynamics within the "void" region may explain why the peak vorticity appeared to shift away from the center as the vortex aged, suggesting the onset of instability. The swirl and axial velocities (which reached 44% and 12% of the rotor tip speed, respectively) were found to be asymmetric relative to the vortex center. In particular, the axial flow was composed of two concentrated zones moving in opposite directions. The radial distribution of the circulation rapidly increased in magnitude until reaching a point just beyond the core radius, after which the rate of growth decreased significantly. The core-radius circulation increased slightly with wake age, but the large-radius circulation appeared to remain relatively constant. The radial distributions of swirl velocity and vorticity exhibit self-similar behaviors, especially within the core. The diameter of the vortex core was initially about 10% of the rotor-blade chord, but more than doubled its size after one revolution of the rotor.
Document ID
20030003700
Acquisition Source
Ames Research Center
Document Type
Technical Publication (TP)
Authors
McAlister, Kenneth W.
Heineck, James T.
Date Acquired
September 7, 2013
Publication Date
July 1, 2002
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AD-A406980
NASA/TP-2002-211848
NAS 1.60:211848
AFDD-TR-02-A-001
A-0208212
Report Number: AD-A406980
Report Number: NASA/TP-2002-211848
Report Number: NAS 1.60:211848
Report Number: AFDD-TR-02-A-001
Report Number: A-0208212
Funding Number(s)
PROJECT: RTOP 712-92-43
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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