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Wake vortex encounter hazards criteria for two aircraft classesAn investigation was conducted using a piloted, motion-base simulator to determine wake vortex hazard criteria for two classes of jet transport aircraft. A light business jet and a large multiengine jet transport were represented respectively. The hazard boundaries were determined in terms of the maximum bank angle due to the vortex encounter. Upsets as small as 7 deg in bank angle were considered to be hazardous at breakout altitude (200 ft (61.0 m)) for Instrument Flight Rule (IFR) and at 50 ft (15.2 m) for Visual Flight Rule (VFR) for both aircraft classes. Proximity to the ground was the primary reason for a hazardous rating. This was reflected in the reduction in the maximum bank angle at the hazard boundary and in more consistent ratings as altitude was decreased.
Document ID
19760021118
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Sammonds, R. I.
(NASA Ames Research Center Moffett Field, CA, United States)
Stinnett, G. W., Jr.
(NASA Ames Research Center Moffett Field, CA, United States)
Larsen, W. E.
(FAA Washington, D. C., United States)
Date Acquired
August 8, 2013
Publication Date
June 1, 1976
Subject Category
Air Transportation And Safety
Report/Patent Number
A-6493
FAA-RD-75-206
NASA-TM-X-73113
Report Number: A-6493
Report Number: FAA-RD-75-206
Report Number: NASA-TM-X-73113
Accession Number
76N28206
Funding Number(s)
PROJECT: RTOP 505-08-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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