1973
DOI: 10.1017/s0022112073000649
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The effects of wake splitter plates on the flow past a circular cylinder in the range 104<R<5×104

Abstract: Experiments were carried out using models having L/D [les ] 2 and the resulting pressure distributions and vortex shedding characteristics are presented. A simple visualization technique which provides explanations of some of the measured results is described. It is concluded that splitter planes reduce the drag markedly by stabilizing the separation points and produce a wake narrower than that for a plain cylinder, raise the base pressure by as much as 50% and affect the Strouhal number to a lesser degree… Show more

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Cited by 290 publications
(122 citation statements)
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“…A two-component laser Doppler anemometer ͑LDA͒, i.e., Dantec Model 58N40 with an enhanced FVA signal processor, was used to measure the mean velocities ͑Ū , V , and W ͒ and their fluctuating components ͑u, v, and w͒ across the wake at x / d =2. 5,4,5,6,8,10,15,20,30,40. The coordinate system ͑x , y , z͒ has already been defined in Fig.…”
Section: B Experimental Detailsmentioning
confidence: 99%
“…A two-component laser Doppler anemometer ͑LDA͒, i.e., Dantec Model 58N40 with an enhanced FVA signal processor, was used to measure the mean velocities ͑Ū , V , and W ͒ and their fluctuating components ͑u, v, and w͒ across the wake at x / d =2. 5,4,5,6,8,10,15,20,30,40. The coordinate system ͑x , y , z͒ has already been defined in Fig.…”
Section: B Experimental Detailsmentioning
confidence: 99%
“…From his study, he showed that it decreased for L/D < 1, where L is the plate length, but it increased for 1 < L/D < 2. Apelt et al [16,17] conducted experiments at Re from 1 × 10 4 to 5 × 10 4 to study the influence of the splitter plate. They concluded that the vortex shedding disappeared when L/D > 5.…”
Section: Introductionmentioning
confidence: 99%
“…The splitter-plate exerts passive control on the dynamics of the near wake (Kwon and Choi 1996;Akilli, Sahin and Filiz Tumen 2005;Tiwari et al 2005) modifying the wake flow in such a manner that VIV suppression is possible. Owing to the presence of the wake splitter-plate, the rolling up of the shear layers is postponed and the subsequent formation of the largescale vortices of the near wake is forced to occur at locations farther downstream (Apelt, West and Szewczyk 1973;Anderson and Szewczyk 1997), thus mitigating the …”
Section: Introductionmentioning
confidence: 99%