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Crosswind Shear Gradient Affect on Wake VorticesParametric simulations with a Large Eddy Simulation (LES) model are used to explore the influence of crosswind shear on aircraft wake vortices. Previous studies based on field measurements, laboratory experiments, as well as LES, have shown that the vertical gradient of crosswind shear, i.e. the second vertical derivative of the environmental crosswind, can influence wake vortex transport. The presence of nonlinear vertical shear of the crosswind velocity can reduce the descent rate, causing a wake vortex pair to tilt and change in its lateral separation. The LES parametric studies confirm that the vertical gradient of crosswind shear does influence vortex trajectories. The parametric results also show that vortex decay from the effects of shear are complex since the crosswind shear, along with the vertical gradient of crosswind shear, can affect whether the lateral separation between wake vortices is increased or decreased. If the separation is decreased, the vortex linking time is decreased, and a more rapid decay of wake vortex circulation occurs. If the separation is increased, the time to link is increased, and at least one of the vortices of the vortex pair may have a longer life time than in the case without shear. In some cases, the wake vortices may never link.
Document ID
20110013647
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Proctor, Fred H.
(NASA Langley Research Center Hampton, VA, United States)
Ahmad, Nashat N.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 25, 2013
Publication Date
June 27, 2011
Subject Category
Aerodynamics
Report/Patent Number
AIAA Paper 2011-3038
NF1676L-11746
Report Number: AIAA Paper 2011-3038
Report Number: NF1676L-11746
Meeting Information
Meeting: 3rd AIAA Atmospheric Space Environments Conference
Location: Honolulu, HI
Country: United States
Start Date: June 27, 2011
End Date: June 30, 2011
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 411931.02.61.07.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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