2000
DOI: 10.1006/jfls.1999.0255
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Vortex-Excited Vibrations of Uniform Pivoted Cylinders in Uniform and Shear Flow

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Cited by 24 publications
(24 citation statements)
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“…The vortex shedding frequency and thus the timing of fluid forcing at different sections along the span of pivoted cylinders is not necessarily consistent. Distinct change in the predominant vortex shedding frequency along the span of pivoted circular cylinders has been found to occur (Balasubramanian et al 2000). In close proximity to the cylinder pivot, the vortex shedding occurred primarily at the Strouhal frequency and, along the majority of the span, shedding frequency was controlled by the cylinder oscillation frequency during the VIV synchronization region.…”
Section: Introductionmentioning
confidence: 93%
See 1 more Smart Citation
“…The vortex shedding frequency and thus the timing of fluid forcing at different sections along the span of pivoted cylinders is not necessarily consistent. Distinct change in the predominant vortex shedding frequency along the span of pivoted circular cylinders has been found to occur (Balasubramanian et al 2000). In close proximity to the cylinder pivot, the vortex shedding occurred primarily at the Strouhal frequency and, along the majority of the span, shedding frequency was controlled by the cylinder oscillation frequency during the VIV synchronization region.…”
Section: Introductionmentioning
confidence: 93%
“…no splitter-plate) circular cylinder, that by definition has non-uniform spanwise vibration amplitudes (see e.g. Balasubramanian et al 2000;Fleming and Williamson 2005;Voorhees et al 2008;Kheirkhah, Yarusevych and Narasimhan 2012). However, to the present authors' knowledge, little, if any, studies exist that have investigated the vibration response of the pivoted rigid circular cylinder with attached wake splitter-plate.…”
Section: Introductionmentioning
confidence: 97%
“…(5) has been introduced by Skop and Balasubramanian [16] to account for the fluctuation of lift coefficient. By following the extended study on sheared flows by Balasubramanian et al [17], the empirical wake variable Q in Eq. (5) is governed by the following van der Pol diffusive wake oscillator ( )…”
Section: Nonlinear Equations Of Riser Motion and Wake Oscillatormentioning
confidence: 99%
“…where C L0 is the lift coefficient of fixed cylinder, F and G are the scaling wake coefficients, and τ is the diffusion parameter which is given, based on a few experimental results, by [17] ( )…”
Section: Nonlinear Equations Of Riser Motion and Wake Oscillatormentioning
confidence: 99%
“…Investigators focusing on this method include Goswami et al (1993b) and Skop & Balasubramanian (1995a,b). Balasubramanian & Skop (1999) reported improved results when including a stall parameter with the van der Pol oscillator. Barhoush et al (1995) combined a van der Pol oscillator approach with a two-dimensional finite element mesh, resulting in a good representation of steady-state vortex-induced vibration behaviour at 'high computational cost'.…”
Section: (I) Wake-body Coupled Modelsmentioning
confidence: 99%