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Vortex breakdown on slender sharp-edged wingsVortex breakdown on slender sharp edged and modified delta wings with varying sweep angles investigated in wind tunnel using schlieren system for flow visualization
Document ID
19710041331
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Kohlman, D. L.
Wentz, W. H., Jr.
Date Acquired
August 6, 2013
Publication Date
March 1, 1971
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 69-778
Report Number: AIAA PAPER 69-778
Meeting Information
Meeting: AIRCRAFT DESIGN AND OPERATIONS MEETING
Location: LOS ANGELES, CA
Start Date: July 14, 1969
End Date: July 16, 1969
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
71A22028
Funding Number(s)
CONTRACT_GRANT: NGR-17-001-043
Distribution Limits
Public
Copyright
Other

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