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Piloted Simulation Study of Wake EncountersThe objective of this current research is to determine an acceptable level of vortex roll disturbance for worst-case encounter geometries during normal, routine operations. This includes: determining the boundary & metric(s), and defining evaluation factors & procedures. The discussion includes: simulation hardware, research simulator software, and research approach & observations.
Document ID
19980073299
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Stewart, Eric
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
August 18, 2013
Publication Date
November 1, 1997
Publication Information
Publication: Proceedings of the NASA First Wake Vortex Dynamic Spacing Workshop
Subject Category
Air Transportation And Safety
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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