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Longitudinal afterbody grooves and shoulder radiusing for low-speed bluff body drag reductionA new low-speed drag reduction approach is proposed which employs longitudinal surface V-shaped grooves cutting through the afterbody shoulder region. The test Reynolds number range was from 20,000 to 200,000 based on undisturbed free-stream flow and a body diameter of 6.08 cm. The V-grooves are shown to be most effective in reducing drag when the afterbody shoulder radius is zero. Reductions in drag of up to 33% have been measured for this condition. For large shoulder radius, the grooves are only effective at the lower Reynolds numbers of the test.
Document ID
19820041033
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Howard, F. G.
(NASA Langley Research Center Hampton, VA, United States)
Quass, B. F.
(NASA Langley Research Center Hampton, VA, United States)
Weinstein, L. M.
(NASA Langley Research Center Hampton, VA, United States)
Bushnell, D. M.
(NASA Langley Research Center High-Speed Aerodynamics Div., Hampton, VA, United States)
Date Acquired
August 10, 2013
Publication Date
November 1, 1981
Subject Category
Aerodynamics
Report/Patent Number
ASME PAPER 81-WA/FE-5
Meeting Information
Meeting: Winter Annual Meeting
Location: Washington, DC
Start Date: November 15, 1981
End Date: November 20, 1981
Sponsors: American Society of Mechanical Engineers
Accession Number
82A24568
Distribution Limits
Public
Copyright
Other

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