Published December 1993
| public
Journal Article
Experiments on flow past rough circular cylinders at large Reynolds numbers
- Creators
- Shih, W. C. L.
- Wang, C.
- Coles, D.
- Roshko, A.
Abstract
Data have been obtained in the 12-foot pressurized wind tunnel at NASA Ames Research Center on flow past smooth and rough circular cylinders at high Reynolds numbers. Steady and unsteady surface pressures were measured around and along the cylinders. Analysis of the results provides lift and drag coefficients and Strouhal numbers for cylinders of several roughness at Reynolds numbers up to 8 × 10^6.
Additional Information
© 1993 Elsevier Science Publishers B.V. This research was sponsored by the Office of Naval Research under contracts N00014-85-C-0764 and N00014-86-C-0882. The technical monitor was Dr. Eugene Silva.Additional details
- Eprint ID
- 38373
- DOI
- 10.1016/0167-6105(93)90030-R
- Resolver ID
- CaltechAUTHORS:20130509-075105354
- N00014-85-C-0764
- Office of Naval Research (ONR)
- N00014-86-C-0882
- Office of Naval Research (ONR)
- Created
-
2013-05-09Created from EPrint's datestamp field
- Updated
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2021-11-09Created from EPrint's last_modified field
- Caltech groups
- GALCIT