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On leading edge vortex and its controlA simple model for the leading edge vortex and a postulation for the existence of a critical vorticity concentration above which a stable leading edge vortex cannot be maintained were proposed. Using the model and postulation, various aspects of vortex control by blowing were discussed. Blowing can be envisioned as a means to control the effective sweep and span of a delta wing by redistributing the vorticity. Mixing between the blowing jet and the vortex has a major effect on the effectiveness of controlling the vortex. Different positioning of one vortex relative to another can either enhance or delay the breakdown of the vortices.
Document ID
19890061681
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ng, T. T.
(Eidetics International, Inc. Torrance, CA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 89-3346
Report Number: AIAA PAPER 89-3346
Meeting Information
Meeting: AIAA Atmospheric Flight Mechanics Conference
Location: Boston, MA
Country: United States
Start Date: August 14, 1989
End Date: August 16, 1989
Sponsors: AIAA
Accession Number
89A49052
Funding Number(s)
CONTRACT_GRANT: NAS2-12989
Distribution Limits
Public
Copyright
Other

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