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Surface flow patterns on an ogive-cylinder at incidenceA set of photographs has been obtained which documents the oil-imaged surface flow patterns of an ogive-cylinder at angles-of-attack between 30 and 85 deg, and Reynolds number of 26,000. Attention is given to the possibility that the bistable nature of the flow within the 50-65 deg angle-of-attack range is linked to the coincident appearance of foci in the surface flow patterns, in view of the suggestion that these foci act as the anchor points allowing the forebody vortical structures to roll up and form the forebody's trailing vortex system.
Document ID
19920038138
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Degani, David
(NASA Ames Research Center Moffett Field, CA, United States)
Tobak, Murray
(NASA Ames Research Center Moffett Field, CA, United States)
Zilliac, G. G.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Publication Information
Publication: AIAA Journal
Volume: 30
ISSN: 0001-1452
Subject Category
Aerodynamics
Report/Patent Number
ISSN: 0001-1452
Accession Number
92A20762
Distribution Limits
Public
Copyright
Other

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