1995
DOI: 10.2208/jscej.1995.525_171
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An Experimental Study on the Control of the Vortex-Induced Vibration of a Circular Cylinder by Acoustic Excitation

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Cited by 4 publications
(2 citation statements)
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“…The numerical results (Suzuki 1999) show that the acoustic excitation at an appropriate frequency dynamically suppresses the leading edge separation and causes a change of vortex structure of a flow around an airfoil. For a circular cylinder, the most effective sound frequency in reducing the vortex-induced oscillation amplitude approximately corresponded to the transition wave frequency predicted by Wei's formula (Hiejima 1996(Hiejima , 1997.…”
Section: Introductionsupporting
confidence: 58%
“…The numerical results (Suzuki 1999) show that the acoustic excitation at an appropriate frequency dynamically suppresses the leading edge separation and causes a change of vortex structure of a flow around an airfoil. For a circular cylinder, the most effective sound frequency in reducing the vortex-induced oscillation amplitude approximately corresponded to the transition wave frequency predicted by Wei's formula (Hiejima 1996(Hiejima , 1997.…”
Section: Introductionsupporting
confidence: 58%
“…Hijima et al [17] investigated numerically the effect of the sound wave with specified frequency on the stability of the separated shear layer around the cylinder. In addition, experimental studies by Hijima et al [18] indicate that the vortex induced vibration of a circular cylinder can be suppressed using the stimulation of the separated shear layer by an acoustic wave with the frequency of the transition waves. Apparently, this method is examined only for small amplitude of the vortex-induced vibration.…”
Section: Introductionmentioning
confidence: 99%