NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
DFW microburst model based on AA-539 dataAnalysis of the August 2, 1985 crash for an L-1011 jumbo jet (DL-191) on approach to the Dallas-Ft. Worth International Airport (DFW) in a thunderstorm indicates that the severe windshear microburst that caused the crash was composed not only of a strong downflow and outflow but also included several large-scale vortex rings entrained in the flowfield. This paper presents a detailed two-dimensional model of the DFW microburst based on data from the MD-80 (AA-539) that followed behind DL-191 and flew through the microburst about two minutes after the crash of DL-191. The model was developed using wind-vector and flight-path data reconstructed by NASA Ames Research Center and a combination of interactive graphics and least-squares error best fit between the modeled and measured wind vectors along the AA-539 flight path. The model indicates that the flowfield contains some significant elements and vortices not previously reported. The alternating direction of rotation of the vortices in the model suggests a microburst structure based on a von Karman vortex street rather than on a Kelvin-Helmholtz instability. The model also indicates that the reconstructed wind-vector data contain a time lag of at least one second in the horizontal winds.
Document ID
19910041490
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Grantham, Walter J.
(Washington State Univ. Pullman, WA, United States)
Roetcisoender, Guy G.
(Washington State University Pullman, United States)
Parks, Edwin K.
(Arizona, University Tucson, United States)
Date Acquired
August 14, 2013
Publication Date
November 1, 1990
Publication Information
Publication: Journal of Aircraft
Volume: 27
ISSN: 0021-8669
Subject Category
Meteorology And Climatology
Accession Number
91A26113
Funding Number(s)
CONTRACT_GRANT: NCA2-216
CONTRACT_GRANT: NCC2-329
Distribution Limits
Public
Copyright
Other

Available Downloads

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