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On a criterion for vortex breakdownA criterion for the onset of vortex breakdown is proposed. Based upon previous experimental, computational, and theoretical studies, an appropriately defined local Rossby number is used to delineate the region where breakdown occurs. In addition, new numerical results are presented which further validate this criterion. A number of previous theoretical studies concentrating on inviscid standing-wave analyses for trailing wing-tip vortices are reviewed and reinterpreted in terms of the Rossby number criterion. Consistent with previous studies, the physical basis for the onset of breakdown is identified as the ability of the flow to sustain such waves. Previous computational results are reviewed and re-evaluated in terms of the proposed breakdown criterion. As a result, the cause of breakdown occurring near the inflow computational boundary, common to several numerical studies, is identified. Finally, previous experimental studies of vortex breakdown for both leading edge and trailing wing-tip vortices are reviewed and quantified in terms of the Rossby number criterion.
Document ID
19870008595
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Spall, R. E.
(Old Dominion Univ. Norfolk, Va., United States)
Gatski, T. B.
(NASA Langley Research Center Hampton, VA, United States)
Grosch, C. H.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1987
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
ICASE-87-3
NAS 1.26:178232
NASA-CR-178232
Report Number: ICASE-87-3
Report Number: NAS 1.26:178232
Report Number: NASA-CR-178232
Accession Number
87N18028
Funding Number(s)
PROJECT: RTOP 505-90-21-01
CONTRACT_GRANT: NAS1-18107
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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