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Wind and Structures Volume 6, Number 5, September 2003, pages 347-356 DOI: https://doi.org/10.12989/was.2003.6.5.347 |
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Drag reduction of a circular cylinder at subcritical flow regime using base shield plates |
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Nabil A.H. EL-Khairy
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| Abstract | ||
| Experimental studies on drag reduction of a circular cylinder of diameter D were conducted in the subcritical flow regime at Reynolds numbers in the range 4 | ||
| Key Words | ||
| drag reduction; circular cylinder; shield plates; base cavity; separation; wake. | ||
| Address | ||
| Department of Civil Engineering, University of Jordan, Amman, Jordan | ||