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Hazard criteria for wake vortex encountersA piloted, motion-base simulation was conducted to evaluate the ability of simulators to produce realistic vortex encounters and to develop criteria to define hazardous encounters. Evaluation of the simulation by pilots experienced in vortex encounters confirmed the capability of the simulator to realistically reproduce wake vortex encounters. A boundary for encounter hazard based on subjective pilot opinion was identified in terms of maximum bank angle. For encounter altitudes from 200 to 500 ft (61.0 to 152.4 m), tentative hazard criteria established for visual flight conditions indicated that the acceptable upset magnitude increased nearly linearly with increasing altitude. The data suggest that the allowable upsets under instrument conditions no greater than 50 percent of that allowable under visual conditions.
Document ID
19760003981
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)
Date Acquired
September 3, 2013
Publication Date
August 1, 1975
Subject Category
Air Transportation And Safety
Report/Patent Number
A-6232
NASA-TM-X-62473
Report Number: A-6232
Report Number: NASA-TM-X-62473
Accession Number
76N11069
Funding Number(s)
PROJECT: RTOP 505-08-21-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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