54th AIAA Aerospace Sciences Meeting 2016
DOI: 10.2514/6.2016-0573
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Flow around a Finite Circular Cylinder Coated with Porous Media

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Cited by 13 publications
(7 citation statements)
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“…Therefore, the outer diameters are chosen to be D = 96 mm with an inner bare diameter of d = 64 mm and thus the ratio of the porous coating thickness to the bare cylinder diameter, t d, is 0.25. This t d ratio is consistent with the aeroacoustic investigation presented in Arcondoulis et al [7] and within the typical t d range of others [1,3,4,8,9,12,15,18]. It is also important to ensure that the Reynolds number range is within the range of previously published data for comparative purposes.…”
Section: A Diameter and Coating Thickness Selectionsupporting
confidence: 88%
“…Therefore, the outer diameters are chosen to be D = 96 mm with an inner bare diameter of d = 64 mm and thus the ratio of the porous coating thickness to the bare cylinder diameter, t d, is 0.25. This t d ratio is consistent with the aeroacoustic investigation presented in Arcondoulis et al [7] and within the typical t d range of others [1,3,4,8,9,12,15,18]. It is also important to ensure that the Reynolds number range is within the range of previously published data for comparative purposes.…”
Section: A Diameter and Coating Thickness Selectionsupporting
confidence: 88%
“…The Reynolds number range of interest is based on published data of both porous coated [2,4,5,6,8,12,13,19,24] and bare cylinders [16,25,26,27] corresponding to Reav,min0.8×105 to Reav,max1.5×105. Therefore a value of D is required such that a similar Reynolds number range could be obtained while also producing shedding tones that are above the anechoic limits of the wind tunnel (approximately 200 Hz) and well-exceed the background noise (that typically decreases with increasing frequency).…”
Section: Methodsmentioning
confidence: 99%
“…There is good agreement on the impact of a full porous coating on the wake of a cylinder, with the wake being stabilised due to the reduction or the delay of vortex shedding [2,[9][10][11][12][13][14][15][16][17][18][19]. Consequently, many studies concluded that the porous coating reduced the fluctuation of aerodynamic forces [2,9,10,[17][18][19].…”
Section: Introductionmentioning
confidence: 99%
“…Consequently, many studies concluded that the porous coating reduced the fluctuation of aerodynamic forces [2,9,10,[17][18][19]. With regard to drag reduction, there has been some discrepancy in the results with some studies finding an increase in drag [2,9,[14][15][16][17]20,21] and others finding a decrease in drag [11,12,[17][18][19]21].…”
Section: Introductionmentioning
confidence: 99%