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The application of laser Doppler velocimetry to trailing vortex definition and alleviationA laser Doppler velocimeter whose focal volume can be rapidly traversed through a flowfield has been used to overcome the problem introduced by excursions of the central vortex filament within a wind tunnel test section. The basic concepts of operation of the instrument are reviewed and data are presented which accurately define the trailing vortex from a square-tipped rectangular wing. Measured axial and tangential velocity distributions are given, both with and without a vortex dissipator panel installed at the wing tip. From the experimental data, circulation and vorticity distributions are obtained and the effect of turbulence injection into the vortex structure is discussed.
Document ID
19730013721
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Orloff, K. L.
(NASA Ames Research Center Moffett Field, CA, United States)
Grant, G. R.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1973
Subject Category
Masers
Report/Patent Number
NASA-TM-X-62243
Accession Number
73N22448
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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