2007
DOI: 10.1007/bf03181894
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Visualization of turbulent flow around a sphere at subcritical reynolds numbers

Abstract: The shear layer evolution and turbulent structure of near-wake behind a sphere at Re = 11,000 and 5,300 were investigated using a smoke-wire visualization method. A laminar flow separation was found to occur near the equator. The smooth laminar shear layers appeared to be axisymmetrically stable to the downstream location of about x/d = 1.0 at Re = 11,000 and x/d = 1.7∼1.8 at Re = 5,300, respectively. At Re = 11,000, the vortex ring-shaped protrusions were observed with the onset of shear layer instability. Mo… Show more

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Cited by 14 publications
(4 citation statements)
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“…The large-scale motions are associated (among other phenomena) to wake meandering [17,26], while the development of small-scale structures (e.g., sub-rotor, f d/U ≥ 5) is due to the production of the turbulence kinetic energy induced in the shear layer of the wake. Similar phenomena have been reported for other setups, including flow passing circular and rectangular cylinders, spheres, among others [27][28][29]. The differences between the cases across scales are highlighted with the corresponding pre-multiplied spectra f Φ in Figure 3(a2-c2).…”
Section: Background Turbulence Modulation On the Wake Velocity Spectrasupporting
confidence: 81%
“…The large-scale motions are associated (among other phenomena) to wake meandering [17,26], while the development of small-scale structures (e.g., sub-rotor, f d/U ≥ 5) is due to the production of the turbulence kinetic energy induced in the shear layer of the wake. Similar phenomena have been reported for other setups, including flow passing circular and rectangular cylinders, spheres, among others [27][28][29]. The differences between the cases across scales are highlighted with the corresponding pre-multiplied spectra f Φ in Figure 3(a2-c2).…”
Section: Background Turbulence Modulation On the Wake Velocity Spectrasupporting
confidence: 81%
“…The time interval between two pulses, t, was controlled by adjusting the delay generator. The FFT-based cross-correlation PIV technique was employed to calculate the velocity from the consecutive particle images (Jang and Lee, 2007). The size of the interrogation window was 32 32 pixels 2 , and each interrogation window was overlapped 50%.…”
Section: Experimental Methodsmentioning
confidence: 99%
“…Most have focused on the vortex shedding phenomena, using hot-wire anemometry to measure the dominant shedding frequencies. They have also studied wake structures, using qualitative flow visualization methods [1][2][3][4][5][6][7].…”
Section: Introductionmentioning
confidence: 99%