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Numerical modeling studies of wake vortex transport and evolution within the planetary boundary layerThe proposed research involves four tasks. The first of these is to simulate accurately the turbulent processes in the atmospheric boundary layer. TASS was originally developed to study meso-gamma scale phenomena, such as tornadic storms, microbursts and windshear effects in terminal areas. Simulation of wake vortex evolution, however, will rely on appropriate representation of the physical processes in the surface layer and mixed layer. This involves two parts. First, a specified heat flux boundary condition must be implemented at the surface. Using this boundary condition, simulation results will be compared to experimental data and to other model results for validation. At this point, any necessary changes to the model will be implemented. Next, a surface energy budget parameterization will be added to the model. This will enable calculation of the surface fluxes by accounting for the radiative heat transfer to and from the ground and heat loss to the soil rather than simple specification of the fluxes. The second task involves running TASS with prescribed wake vortices in the initial condition. The vortex models will be supplied by NASA Langley Research Center. Sensitivity tests will be performed on different meteorological environments in the atmospheric boundary layer, which include stable, neutral, and unstable stratifications, calm and severe wind conditions, and dry and wet conditions. Vortex strength may be varied as well. Relevant non-dimensional parameters will include the following: Richardson number or Froude number, Bowen ratio, and height to length scale ratios. The model output will be analyzed and visualized to better understand the transport, decay, and growth rates of the wake vortices. The third task involves running simulations using observed data. MIT Lincoln Labs is currently planning field experiments at the Memphis airport to measure both meteorological conditions and wake vortex characteristics. Once this data becomes available, it can be used to validate the model for vortex behavior under different atmospheric conditions. The fourth task will be to simulate the wake in a more realistic environment covering a wider area. This will involve grid nesting, since high resolution will be required in the wake region but a larger total domain will be used. During the first allocation year, most of the first task will be accomplished.
Document ID
19940031016
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lin, Yuh-Lang
(North Carolina State Univ. Raleigh, NC, United States)
Arya, S. Pal
(North Carolina State Univ. Raleigh, NC, United States)
Kaplan, Michael L.
(North Carolina State Univ. Raleigh, NC, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1994
Subject Category
Air Transportation And Safety
Report/Patent Number
NAS 1.26:196078
NASA-CR-196078
Report Number: NAS 1.26:196078
Report Number: NASA-CR-196078
Accession Number
94N35522
Funding Number(s)
CONTRACT_GRANT: NCC1-188
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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