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Calculations of axisymmetric vortex sheet roll-up using a panel and a filament modelA method for calculating the self-induced motion of a vortex sheet using discrete vortex elements is presented. Vortex panels and vortex filaments are used to simulate two-dimensional and axisymmetric vortex sheet roll-up. A straight forward application using vortex elements to simulate the motion of a disk of vorticity with an elliptic circulation distribution yields unsatisfactroy results where the vortex elements move in a chaotic manner. The difficulty is assumed to be due to the inability of a finite number of discrete vortex elements to model the singularity at the sheet edge and due to large velocity calculation errors which result from uneven sheet stretching. A model of the inner portion of the spiral is introduced to eliminate the difficulty with the sheet edge singularity. The model replaces the outermost portion of the sheet with a single vortex of equivalent circulation and a number of higher order terms which account for the asymmetry of the spiral. The resulting discrete vortex model is applied to both two-dimensional and axisymmetric sheets. The two-dimensional roll-up is compared to the solution for a semi-infinite sheet with good results.
Document ID
19860020295
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Kantelis, J. P.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Widnall, S. E.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1986
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-177081
FDRL-86-1
NAS 1.26:177081
Report Number: NASA-CR-177081
Report Number: FDRL-86-1
Report Number: NAS 1.26:177081
Accession Number
86N29767
Funding Number(s)
CONTRACT_GRANT: NAG2-251
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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