Flow Around a Rotatable Circular Cylinder-Plate Body at Subcritical Reynolds Numbers
Author:
Affiliation:
1. Karadeniz Technical University, 61080 Trabzon, Turkey
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.4265
Reference22 articles.
1. Supercritical Reynolds number experiments on a freely rotatable cylinder/splitter plate body
2. Effects of a splitter plate on the near wake of a circular cylinder in 2 and 3-dimensional flow configurations
3. Vortex suppression of the cylinder wake by deflectors
4. Effects of splitter plates on the wake flow behind a bluff body
5. VORTEX SHEDDING FROM BLUFF BODIES WITH SPLITTER PLATES
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