2022
DOI: 10.1016/j.oceaneng.2022.111574
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Effect of initial roll or pitch angles on the vortex-induced motions (VIM) of floating circular cylinders with a low aspect ratio

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Cited by 5 publications
(4 citation statements)
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“…4 that vortical structures leaving the computational domain at x∕D = 35 re-enter the Eulerian complementary domain at x∕D = 0.0 due to the periodic boundary conditions imposed by the Fourier pseudo-spectral method (FPSM). Simultaneously, it is noted that these vortical structures are attenuated until their complete extinction, (19) k j ûj = 0 facilitated by the use of both buffer and forcing zones. The imposition of periodic boundary conditions is the main challenge when working with the FPSM.…”
Section: Cylinder Anchored With a Spring-damper System Verticalmentioning
confidence: 99%
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“…4 that vortical structures leaving the computational domain at x∕D = 35 re-enter the Eulerian complementary domain at x∕D = 0.0 due to the periodic boundary conditions imposed by the Fourier pseudo-spectral method (FPSM). Simultaneously, it is noted that these vortical structures are attenuated until their complete extinction, (19) k j ûj = 0 facilitated by the use of both buffer and forcing zones. The imposition of periodic boundary conditions is the main challenge when working with the FPSM.…”
Section: Cylinder Anchored With a Spring-damper System Verticalmentioning
confidence: 99%
“…According to [48], FIV, in single phase flows, is classified into three types based on excitation characteristics: extraneously-induced excitation (EIE), instability-induced excitation (IIE) and motioninduced excitation (MIE). Each excitation can lead to four distinct phenomena: vortex-induced-vibration (VIV), vortex-induced-motion (VIM), wake-induced-vibration (WIV), galloping and flutter [14,19,42].…”
Section: Introductionmentioning
confidence: 99%
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“…The effects of initial roll or pitch angles on the VIM amplitudes of a floating circular cylinder with a low aspect ratio (m * = 1, A R = 1.5) were investigated experimentally [74], with Reynolds numbers from 1.2 × 10 4 to 1.0 × 10 5 . The reduced velocity varied from 1 to 12.…”
Section: Model Tests On Sparmentioning
confidence: 99%