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The Breakup of Trailing-Line VorticesIt is now known that Batchelor's trailing-line vortex is extremely unstable to small amplitude disturbances for swirl numbers in the neighborhood of 0.83. The results of numerical calculations are presented that show the response of the vortex in this range of swirl numbers to finite amplitude, temporal, helical disturbances. Phenomena observed include: (1) ejection of axial vorticity and momentum from the core resulting in the creation of secondary, separate vortices; (2) a great intensification of core axial vorticity and a weakening of core momentum; and (3) the production of azimuthal vorticity in the form of a tightly wrapped spiral wave. The second phenomenon eventually stablizes the vortex, which then smooths and gradually returns to an axisymmetric state. The calculations are mixed spectral-finite-difference, fourth-order accurate, and have been carried out at Reynolds numbers of 1000 to 2000. Some linearized results are also discussed in an attempt to explain the process of vortex intensification.
Document ID
19910001554
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
David Jacqmin
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1989
Publication Information
Publication: NASA Computational Fluid Dynamics Conference. Volume 1: Sessions 1-6
Publisher: National Aeronautics and Space Administration
Volume: 1
Subject Category
Aerodynamics
Report/Patent Number
NASA/CP-10038-VOL-1
Meeting Information
Meeting: NASA Computational Fluid Dynamics Conference
Location: Moffett Field, CA
Country: US
Start Date: March 7, 1989
End Date: March 9, 1989
Sponsors: National Aeronautics and Space Administration
Accession Number
91N10867
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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