2016
DOI: 10.1007/s00348-016-2119-7
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Circular cylinders with soft porous cover for flow noise reduction

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Cited by 72 publications
(64 citation statements)
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References 32 publications
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“…Finally, the data were converted to power spectral densities L p re 20 µPa. The experimental setup is shown in Figure 1(a) and explained in more detail in [5]. In addition to the acoustic measurements from [5], constant temperature anemometry (CTA) measurements were performed in the wake of the cylinders at a single flow speed using a Dantec single-wire P11 probe.…”
Section: Iia Setupmentioning
confidence: 99%
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“…Finally, the data were converted to power spectral densities L p re 20 µPa. The experimental setup is shown in Figure 1(a) and explained in more detail in [5]. In addition to the acoustic measurements from [5], constant temperature anemometry (CTA) measurements were performed in the wake of the cylinders at a single flow speed using a Dantec single-wire P11 probe.…”
Section: Iia Setupmentioning
confidence: 99%
“…In addition to a reduction of noise, such materials also affect the flow around the cylinder and, subsequently, the aerodynamic drag [12][13][14][15][16][17][18][19][20]. In a previous experimental study by the authors [5], the noise reducing effects of a large number of different flow permeable cylinder covers were shown. Thereby, the cylinder models consisted of a non-porous core cylinder on which hollow cylinder disks made of porous material were threaded.…”
Section: Introductionmentioning
confidence: 99%
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“…The setup and methodology used for the measurement of the flow noise generated by the cylinders is basically identical to that used in the study by Geyer and Sarradj [19] on the noise generated by porous covered cylinders. It consists of an aerodynamically closed test section of approximately 1.5 m length that is mounted to the rectangular nozzle of the open jet wind tunnel, which has a contraction ratio of about 31.2 and an exit area of 0.23 m Ö 0.28 m. The nozzle was specifically built for the purpose of transforming the circular cross section of the wind tunnel to a rectangular cross section at the nozzle exit using the design of Morel [20].…”
Section: Wind Tunnelmentioning
confidence: 99%
“…The flow inside the test section can be described as essentially not turbulent, with turbulence intensities in the order of 0.2 % [19] (measured in front of the nozzle without the test section attached). A very low inflow turbulence was desired for the present measurements, since it is known that even small fluctuations may have a significant effect on the flow [21].…”
Section: Wind Tunnelmentioning
confidence: 99%