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Wake Vortex Transport in Proximity to the GroundA sensitivity study for aircraft wake vortex transport has been conducted using a validated large eddy simulation (LES) model. The study assumes neutrally stratified and nonturbulent environments and includes the consequences of the ground. The numerical results show that the nondimensional lateral transport is primarily influenced by the magnitude of the ambient crosswind and is insensitive to aircraft type. In most of the simulations, the ground effect extends the lateral position of the downwind vortex about one initial vortex spacing (b(sub o)) in the downstream direction. Further extension by as much as one b(sub o) occurs when the downwind vortex remains 'in ground effect' (IGE) for relatively long periods of time. Results also show that a layer-averaged ambient wind velocity can be used to bound the time for lateral transport of wake vortices to insure safe operations on a parallel runway.
Document ID
20000109955
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Hamilton, David W.
(NASA Langley Research Center Hampton, VA United States)
Proctor, Fred H.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2000
Subject Category
Aerodynamics
Meeting Information
Meeting: Digital Avionics Systems
Location: Philadelphia, PA
Country: United States
Start Date: October 7, 2000
End Date: October 13, 2000
Sponsors: American Inst. of Aeronautics and Astronautics, Institute of Electrical and Electronics Engineers
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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