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Investigation of compressible vortex flow characteristicsThe nature of intense air vortices was studied and the factors which determine the intensity and rate of decay of both single and pairs of vortices were investigated. Vortex parameters of axial pressure differential, circulation, outflow rates, separation distance and directions of rotation were varied. Unconfined vortices, generated by a single rotating cage, were intensified by an increasing axial pressure gradient. Breakdown occurred when the axial gradient became negligible. The core radius was a function of the axial gradient. Dual vortices, generated by two counterrotating cages, rotated opposite to the attached cages. With minimum spacing only one vortex was formed which rotated in a direction opposite to the attached cage. When one cage rotated at half the speed of the other cage, one vortex formed at the higher speed cage rotating in the cage direction.
Document ID
19780005069
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Muirhead, V. U.
(Kansas Univ. Lawrence, KS, United States)
Date Acquired
September 3, 2013
Publication Date
November 1, 1977
Subject Category
Aerodynamics
Report/Patent Number
CRINC-FRL-260-1
NASA-CR-145261
Report Number: CRINC-FRL-260-1
Report Number: NASA-CR-145261
Accession Number
78N13012
Funding Number(s)
CONTRACT_GRANT: NAS1-12976
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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