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Low-speed vortical flow over a 5-degree cone with tip geometry variationsExperimental results on the surface pressures and sectional side forces on a 5-deg cone were obtained for the cases of three different nose tips. The sectional side force data for both the sharp cone and the blunt nose cone configurations showed a dependence on roll orientation. The blunt nose configurations were found to be effective in reducing the sectional side force for angles of attack up to 25 deg.
Document ID
19890040832
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chu, J.
(NASA Langley Research Center Hampton, VA, United States)
Hall, R. M.
(NASA Langley Research Center Hampton, VA, United States)
Kjelgaard, S. O.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
October 1, 1988
Subject Category
Aerodynamics
Report/Patent Number
SAE PAPER 881422
Report Number: SAE PAPER 881422
Accession Number
89A28203
Distribution Limits
Public
Copyright
Other

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