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Vortex Lift Augmentation by SuctionLift performance is improved on a 60 degrees swept Gothic wing. Vortex lift at moderate to high angles of attack on highly swept wings used to improve takeoff performance and maneuverability. New design proposed in which suction of propulsion system augments vortex. Turbofan placed at down stream end of leading-edge vortex system induces vortex to flow into inlet which delays onset of vortex breakdown.
Document ID
19830000071
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Taylor, A. H.
Jackson, L. R.
Huffman, J. K.
Date Acquired
August 11, 2013
Publication Date
August 1, 1983
Publication Information
Publication: NASA Tech Briefs
Volume: 7
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-12969
Accession Number
83B10071
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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