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Axisymmetric bluff-body drag reduction using circumferential groovesThe effect of shoulder radiusing and circumferentially grooving the afterbodies of bluff bodies to reduce the base drag at low speeds is discussed. Shoulder radii as large as 2.75 body diameters are examined. Reynolds number based on body diameter varied from 20,000 to 200,000. Results indicate that increasing the shoulder radius to 2.75 body diameters can reduce the drag levels to those of a streamline body having 67 percent greater fineness ratio. For zero shoulder radius, circumferential grooves were found to be effective in reducing body drag for zero shoulder radius in both laminar and tripped flow. Circumferential grooves on the afterbody with a shoulder radius of one-half the body diameter were only effective in reducing drag for laminar flow.
Document ID
19830057410
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Howard, F. G.
(NASA Langley Research Center Hampton, VA, United States)
Goodman, W. L.
(NASA Langley Research Center Hampton, VA, United States)
Walsh, M. J.
(NASA Langley Research Center High-Speed Aerodynamics Div., Hampton, VA, United States)
Date Acquired
August 11, 2013
Publication Date
July 1, 1983
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 83-1788
Accession Number
83A38628
Distribution Limits
Public
Copyright
Other

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