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A subvortex technique for the close approach to a discretized vortex sheetThe close-approach problem associated with flow calculation methods based on vortex-lattice theory was examined numerically using two-dimensional discretized vortex sheets. The analysis first yields a near-field radius of approximately the distance apart of the vortices in the lattice; only within this distance from the sheet are the errors arising from the discretization significant. Various modifications to the discrete vortices are then considered with the objective of reducing the errors. This leads to a near-field model in which a vortex splits into an increasing number of subvortices as it is approached. The subvortices, whose strengths vary linearly from the vortex position, are evenly distributed along an interpolated curve passing through the basic vortices. This subvortex technique can be extended to the three-dimensional case and is efficient because the number of vortices is effectively increased, but only where and when needed.
Document ID
19760003959
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Maskew, B.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1975
Subject Category
Aerodynamics
Report/Patent Number
A-6277
NASA-TM-X-62487
Report Number: A-6277
Report Number: NASA-TM-X-62487
Accession Number
76N11047
Funding Number(s)
PROJECT: RTOP 505-06-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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