Drag reduction of flat plate normal to airstream by flow control using a rod
Experimental studies on drag reduction of a flat plate normal to airstream were carried out. To control the flow around the plate, a small rod was set upstream of the plate. The chord length of the plate, D, was 50 mm and the diameter of the rod, d, ranged from 2 to 20 mm, and the distance between t...
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Veröffentlicht in: | Journal of wind engineering and industrial aerodynamics 2002-05, Vol.90 (4), p.359-376 |
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Format: | Artikel |
Sprache: | eng |
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Zusammenfassung: | Experimental studies on drag reduction of a flat plate normal to airstream were carried out. To control the flow around the plate, a small rod was set upstream of the plate. The chord length of the plate,
D, was 50
mm and the diameter of the rod,
d, ranged from 2 to 20
mm, and the distance between the axes of the rod and the plate,
L/
D, was varied from 1.0 to 2.6. The Reynolds number ranged from 1.9×10
4 to 7.7×10
4. For the case without vortex shedding from the rod at
d/
D=0.4 and
L/
D=2.0, the maximum reduction of the total drag coefficient is about 20–30% compared to the drag without the rod in the same range of the Reynolds number. |
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ISSN: | 0167-6105 1872-8197 |
DOI: | 10.1016/S0167-6105(01)00198-2 |