NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Vortex tubes in turbulent flows: Identification, representation, reconstructionIn many cases the structure of a fluid flow is well-characterized by its vortices, especially for the purpose of visualization. In this paper we present a new algorithm for identifying vortices in complex flows. The algorithm produces a skeleton line along the center of a vortex by using a two-step predictor-corrector scheme. The vorticity vector field serves as the predictor and the pressure gradient (in the perpendicular plane) serves as the corrector. We describe an economical description of the vortex tube's cross-section: a 5-term truncated Fourier series is generally sufficient, and it compresses the representation of the flow by a factor of 4000 or more. We reconstruct the vortex tubes as generalized cylinders, providing a polygonal mesh suitable for display on a graphics workstation. We show how the reconstructed geometry of vortex tubes can be enhanced to help visualize helical motion in a static image.
Document ID
19940031485
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Banks, David C.
(Institute for Computer Applications in Science and Engineering Hampton, VA, United States)
Singer, Bart A.
(Institute for Computer Applications in Science and Engineering Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1994
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
ICASE-94-22
NASA-CR-194900
NAS 1.26:194900
AD-A280504
Report Number: ICASE-94-22
Report Number: NASA-CR-194900
Report Number: NAS 1.26:194900
Report Number: AD-A280504
Accession Number
94N35992
Funding Number(s)
CONTRACT_GRANT: NAS1-19299
CONTRACT_GRANT: NAS1-19480
PROJECT: RTOP 505-90-52-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available