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Rotor tip vortex geometry measurements using the wide-field shadowgraph techniqueRotor tip vortex geometry data have been acquired using the wide-field shadowgraph technique. Shadowgraphs were taken of the wakes of two model main-rotor systems in hover. These shadowgraphs provided detailed tip vortex trajectories from which axial and radial vortex coordinates were measured. Using these coordinates, prescribed-wake parameters were determined and input into a hover-performance prediction code. The resultant predictions were compared with experimental performance data to help assess the capabilities of this code. Another result of the experimental work was the development of a method to predict the visibility of rotor tip vortices on shadowgraphs. Using this method, the ability of the shadowgraph technique to visualize tip vortices in the rotor wake was quantified.
Document ID
19860064842
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Norman, T. R.
(NASA Ames Research Center Moffett Field, CA, United States)
Light, J. S.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 12, 2013
Publication Date
June 1, 1986
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 86-1780
Report Number: AIAA PAPER 86-1780
Accession Number
86A49580
Distribution Limits
Public
Copyright
Other

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