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Preliminary flight test investigation of an airborne wake vortex detection conceptNASA and the FAA have conducted a brief flight-test investigation to furnish preliminary data on the feasibility of transport aircraft wake-vortices' detection, with a view to improving airport capacity by reducing the longitudinal in-trail spacing between aircraft on landing runs. Attention was given to the possibility that the detection of strong vortices at a sufficiently early stage might furnish reasonable warning of impending aerodynamic effects. Preliminary results indicate that while maximum detection distances obtainable with wingtip-mounted flow-angularity vanes are slightly lower than had been predicted, improved detector algorithms may render them more sensitive.
Document ID
19900046848
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Verstynen, Harry A.
(NASA Langley Research Center Hampton, VA, United States)
Patterson, James C., Jr.
(Vigyan Research Associates, Inc. Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 90-1282
Meeting Information
Meeting: AIAA/SFTE/DGLR/SETP Biannual Flight Test Conference
Location: Ontario, CA
Country: United States
Start Date: May 22, 1990
End Date: May 24, 1990
Accession Number
90A33903
Distribution Limits
Public
Copyright
Other

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