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Optimization and application of riblets for turbulent drag reductionRiblet surfaces have been tested in boundary layers having different upstream histories and at higher Reynolds numbers than previously reported. The drag reduction for the riblet surfaces was found to be dependent on the height and spacing of the riblets in law-of-the-wall variables regardless of the free-stream Reynolds number or upstream boundary-layer history. Micro-photographs of the actual riblet geometries are examined to determine the effect of rib details on the riblet drag-reduction performances. To further increase drag-reduction performance, riblet surfaces are combined with another drag-reduction concept, the large-eddy breakup device (LEBU). In addition, the yaw sensitivity of riblets is evaluated, as well as the characteristics of riblet surfaces manufactured out of a thin vinyl sheet.
Document ID
19840035252
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Walsh, M. J.
(NASA Langley Research Center Hampton, VA, United States)
Lindemann, A. M.
(NASA Langley Research Center High-Speed Aerodynamics Div., Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 84-0347
Report Number: AIAA PAPER 84-0347
Accession Number
84A18039
Distribution Limits
Public
Copyright
Other

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