TY - JOUR
T1 - Circular cylinders exposed to vortex-induced vibrations in restricted waters
T2 - VIV response from the bottom to the free surface
AU - Duranay, Aytekin
AU - Demirhan, Alkin Erdal
AU - Dobrucali, Erinc
AU - Kinaci, Omer Kemal
N1 - Publisher Copyright:
© 2025
PY - 2025/1
Y1 - 2025/1
N2 - In this paper, we present a comprehensive experimental investigation into the effect of bottom and free surface boundaries on vortex-induced vibrations (VIV) of a freely oscillating circular cylinder. Effects of the boundaries were examined under varying gap ratios between the cylinder and these boundaries at a low mass ratio of mr=0.827, only in the cross-flow direction, in the Reynolds number range of 1.2·104≤Re≤9·104. The gap ratios, varied from −0.75 to 2, correspond to an approximate Froude number (Fr) of around 0.50. We have examined the VIV response of this cylinder through thirteen tests conducted in various stages: near the bottom boundary, at a sufficient distance from all boundaries, close to the free water surface, and partially submerged. The findings show that as the cylinder approaches the free surface, the synchronization range gradually narrows, and the amplitude response diminishes. Within these cases, frequencies deviate from the general trend nearby the end of the synchronization range. Upon the cylinderʼs upper surface contacting or penetrating the free surface, the VIV synchronization starts at a higher non-dimensional velocity. In the cases of piercing cylinders, a wide synchronization range was observed where the submergence of the body was only around 25 %. The cylinders piercing the free surface showcase a distinctive frequency pattern, revealing a nearly-constant trend despite the escalating flow velocity within the synchronization range. Lower amplitude and broader range of synchronization were observed in the experiments close to the bottom boundary. As the cylinder moves further from the bottom, the boundary effect vanishes and the amplitudes get higher.
AB - In this paper, we present a comprehensive experimental investigation into the effect of bottom and free surface boundaries on vortex-induced vibrations (VIV) of a freely oscillating circular cylinder. Effects of the boundaries were examined under varying gap ratios between the cylinder and these boundaries at a low mass ratio of mr=0.827, only in the cross-flow direction, in the Reynolds number range of 1.2·104≤Re≤9·104. The gap ratios, varied from −0.75 to 2, correspond to an approximate Froude number (Fr) of around 0.50. We have examined the VIV response of this cylinder through thirteen tests conducted in various stages: near the bottom boundary, at a sufficient distance from all boundaries, close to the free water surface, and partially submerged. The findings show that as the cylinder approaches the free surface, the synchronization range gradually narrows, and the amplitude response diminishes. Within these cases, frequencies deviate from the general trend nearby the end of the synchronization range. Upon the cylinderʼs upper surface contacting or penetrating the free surface, the VIV synchronization starts at a higher non-dimensional velocity. In the cases of piercing cylinders, a wide synchronization range was observed where the submergence of the body was only around 25 %. The cylinders piercing the free surface showcase a distinctive frequency pattern, revealing a nearly-constant trend despite the escalating flow velocity within the synchronization range. Lower amplitude and broader range of synchronization were observed in the experiments close to the bottom boundary. As the cylinder moves further from the bottom, the boundary effect vanishes and the amplitudes get higher.
KW - Bottom effect
KW - Free surface
KW - Piercing
KW - VIV
KW - Vortex-induced vibrations
UR - http://www.scopus.com/inward/record.url?scp=85215231650&partnerID=8YFLogxK
U2 - 10.1016/j.apor.2025.104430
DO - 10.1016/j.apor.2025.104430
M3 - Article
AN - SCOPUS:85215231650
SN - 0141-1187
VL - 154
JO - Applied Ocean Research
JF - Applied Ocean Research
M1 - 104430
ER -