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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
 


Drag reduction of a circular cylinder at subcritical flow regime using base shield plates
Nabil A.H. EL-Khairy

 
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
 

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