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Vortex maneuver lift for super-cruise configurationsSome of the theoretical and experimental research conducted at the NASA Langley Research Center is presented to investigate the subsonic vortex-lift producing capabilities for two classes of Super-Cruise designs: a close-coupled wing-canard arrangement and a slender wing configuration. In addition, several analytical methods are discussed for estimating critical structural design loads for thin, highly swept wings having separated leading-edge vortex flows.
Document ID
19760014073
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Campbell, J. F. (NASA Langley Research Center Hampton, VA, United States)
Gloss, B. B. (NASA Langley Research Center Hampton, VA, United States)
Lamar, J. E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1976
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-72836
Accession Number
76N21161
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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