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Vortex breakdown on slender sharp-edged wings.Vortex 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
19690057655
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kohlman, D. L.
Wentz, W. H., Jr.
Date Acquired
August 5, 2013
Publication Date
July 1, 1969
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 69-778
Report Number: AIAA PAPER 69-778
Meeting Information
Meeting: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AIRCRAFT DESIGN AND OPERATIONS MEETING
Location: LOS ANGELES, CALIF.
Start Date: July 14, 1969
End Date: July 16, 1969
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
69A35644
Distribution Limits
Public
Copyright
Other

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