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3D visualization of unsteady 2D airplane wake vorticesAir flowing around the wing tips of an airplane forms horizontal tornado-like vortices that can be dangerous to following aircraft. The dynamics of such vortices, including ground and atmospheric effects, can be predicted by numerical simulation, allowing the safety and capacity of airports to be improved. In this paper, we introduce three-dimensional techniques for visualizing time-dependent, two-dimensional wake vortex computations, and the hazard strength of such vortices near the ground. We describe a vortex core tracing algorithm and a local tiling method to visualize the vortex evolution. The tiling method converts time-dependent, two-dimensional vortex cores into three-dimensional vortex tubes. Finally, a novel approach calculates the induced rolling moment on the following airplane at each grid point within a region near the vortex tubes and thus allows three-dimensional visualization of the hazard strength of the vortices. We also suggest ways of combining multiple visualization methods to present more information simultaneously.
Document ID
19950005180
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Ma, Kwan-Liu
(Institute for Computer Applications in Science and Engineering Hampton, VA, United States)
Zheng, Z. C.
(Institute for Computer Applications in Science and Engineering Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1994
Subject Category
Computer Programming And Software
Report/Patent Number
ICASE-94-45
NAS 1.26:194931
NASA-CR-194931
AD-A284745
Report Number: ICASE-94-45
Report Number: NAS 1.26:194931
Report Number: NASA-CR-194931
Report Number: AD-A284745
Accession Number
95N11593
Funding Number(s)
CONTRACT_GRANT: NAG1-1437
PROJECT: RTOP 505-90-52-01
CONTRACT_GRANT: NAS1-19480
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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