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Feasibility of an onboard wake vortex avoidance systemIt was determined that an onboard vortex wake detection system using existing, proven instrumentation is technically feasible. This system might be incorporated into existing onboard systems such as a wind shear detection system, and might provide the pilot with the location of a vortex wake, as well as an evasive maneuver so that the landing separations may be reduced. It is suggested that this system might be introduced into our nation's commuter aircraft fleet and major air carrier fleet and permit a reduction of current landing separation standards, thereby reducing takeoff and departure delays.
Document ID
19910009761
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bilanin, Alan J.
(Continuum Dynamics, Inc. Princeton, NJ, United States)
Teske, Milton E.
(Continuum Dynamics, Inc. Princeton, NJ, United States)
Curtiss, Howard C., Jr.
(Continuum Dynamics, Inc. Princeton, NJ, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1987
Subject Category
Air Transportation And Safety
Report/Patent Number
NASA-CR-187521
NAS 1.26:187521
CDI-87-02
Report Number: NASA-CR-187521
Report Number: NAS 1.26:187521
Report Number: CDI-87-02
Accession Number
91N19074
Funding Number(s)
PROJECT: RTOP 505-68-30-10
CONTRACT_GRANT: DTRS-57-85-C-000123
CONTRACT_GRANT: NAS1-17742
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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