NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Shear-Layer Effects on Trailing VorticesCrosswind shear can influence the trailing vortex trajectories significantly, according to both field measurement and numerical simulations. Point vortex models are used in this paper to study the fluid dynamic mechanism in the interactions between trailing vortex pair and shear layers. It has been shown that the shear-layer deformation causes the vortex descent history difference in the two vortices of the vortex pair. When a shear layer is below the vortex pair with the same sign as the left vortex, the right vortex descends less than the left vortex. When the same shear layer is above the vortex pair, the right vortex descends more. The descent altitudes of the two vortices are the same when they go through a constant, non-deformed shear layer. Those trends are in agreement with Navier-Stokes simulations.
Document ID
19990064495
Acquisition Source
Langley Research Center
Document Type
Reprint (Version printed in journal)
Authors
Zheng, Z. C.
(University of South Alabama Mobile, AL United States)
Baek, K.
(University of South Alabama Mobile, AL United States)
Date Acquired
August 19, 2013
Publication Date
January 1, 1998
Subject Category
Aerodynamics
Report/Patent Number
AIAA Paper 98-0316
Meeting Information
Meeting: Aerospace Sciences
Location: Reno, NV
Country: United States
Start Date: January 12, 1998
End Date: January 15, 1998
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NAG1-1911
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available