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Preliminary results of simulated vortex encounters by a twin-engine, commercial aircraft during final landing approachPiloted simulations of encounters with vortices of various ages and degrees of attenuation were performed with the Visual Motion Simulator. In the simulations, a twin engine, commercial transport on final approach, encountered the modeled vortices of a four engine, wide body, commercial transport. The data show the effect of vortex age and attenuation on the severity of the initial upset, as well as the effect of the vortex encounters on the landing capability.
Document ID
19800017786
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Hastings, E. C., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Holbrook, G. T.
(NASA Langley Research Center Hampton, VA, United States)
Keyser, G. L., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1980
Subject Category
Air Transportation And Safety
Report/Patent Number
NASA-TM-81782
Report Number: NASA-TM-81782
Accession Number
80N26285
Funding Number(s)
PROJECT: RTOP 505-44-23-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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