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Axisymmetric bluff-body drag reduction through geometrical modificationThe effect of shoulder radiusing and grooving (longitudinally and circumferentially) the afterbodies of bluff bodies to reduce the base drag at low speeds is investigated experimentally. Shoulder radii as large as 2.75 body diameters are examined. Reynolds number (ReD) based on body diameter varied from 20,000 to 200,000. Results indicate that increasing the shoulder radius to 2.00 body diameters can reduce the drag levels to those of a streamline body having 67 percent greater fineness ratio. For the relatively sharp shoulder case, body drag reductions as large as 50 and 33 percent are obtained using circumferential or longitudinal grooves, respectively.
Document ID
19850053436
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Howard, F. G.
(NASA Langley Research Center Hampton, VA, United States)
Goodman, W. L.
(NASA Langley Research Center High-Speed Aerospace Div., Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
June 1, 1985
Publication Information
Publication: Journal of Aircraft
Volume: 22
ISSN: 0021-8669
Subject Category
Aerodynamics
Report/Patent Number
ISSN: 0021-8669
Accession Number
85A35587
Distribution Limits
Public
Copyright
Other

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