TY - JOUR
T1 - Vortex-induced vibrations and galloping of a square cylinder: The impact of damping and mass ratio
AU - He, Zongwei
AU - Zhao, Ying
AU - Zhang, Hongfu
AU - Tang, Hui
AU - Zhu, Qingchi
AU - Ai, Yifeng
AU - He, Xuhui
AU - Zhou, Lei
N1 - Publisher Copyright:
© 2025 Elsevier Ltd
PY - 2025/3/15
Y1 - 2025/3/15
N2 - This paper focuses on the effects of the damping ratio and mass ratio on the vortex-induced vibration (VIV) and galloping of a square cylinder through numerical simulations at a Reynolds number 200. Dynamic Mode Decomposition (DMD) is applied to uncover how the damping ratio influences the vortex shedding mode of the cylinder. The results show that for VIV, the vibration amplitude decreases with an increasing damping ratio as is expected, and the corresponding mathematic model is provided. As the damping ratio increases, the mean drag coefficient decreases, while the standard deviation of the fluctuating lift coefficient decreases rapidly before gradually rising, with a knee point at damping ratio 0.23. With increasing damping ratio, the dominant mode changes while the vortex shedding mode remains “2S”. For galloping, the mean drags, vibration amplitude, and fluctuating lift all decrease sharply with rising damping ratio, after which they stabilize. The mathematic model for vibration amplitude and damping ratio is also provided. This inflection point is identified as the critical damping ratio, which regulates the onset of galloping. Across this process, the dominant mode remains M1, while the vortex shedding mode transitions from “P + S” to “2S” as the damping ratio increases.
AB - This paper focuses on the effects of the damping ratio and mass ratio on the vortex-induced vibration (VIV) and galloping of a square cylinder through numerical simulations at a Reynolds number 200. Dynamic Mode Decomposition (DMD) is applied to uncover how the damping ratio influences the vortex shedding mode of the cylinder. The results show that for VIV, the vibration amplitude decreases with an increasing damping ratio as is expected, and the corresponding mathematic model is provided. As the damping ratio increases, the mean drag coefficient decreases, while the standard deviation of the fluctuating lift coefficient decreases rapidly before gradually rising, with a knee point at damping ratio 0.23. With increasing damping ratio, the dominant mode changes while the vortex shedding mode remains “2S”. For galloping, the mean drags, vibration amplitude, and fluctuating lift all decrease sharply with rising damping ratio, after which they stabilize. The mathematic model for vibration amplitude and damping ratio is also provided. This inflection point is identified as the critical damping ratio, which regulates the onset of galloping. Across this process, the dominant mode remains M1, while the vortex shedding mode transitions from “P + S” to “2S” as the damping ratio increases.
KW - Damping ratio
KW - Galloping
KW - Square cylinder
KW - Vortex-induced vibration
UR - http://www.scopus.com/inward/record.url?scp=85214883888&partnerID=8YFLogxK
U2 - 10.1016/j.oceaneng.2025.120371
DO - 10.1016/j.oceaneng.2025.120371
M3 - Journal article
AN - SCOPUS:85214883888
SN - 0029-8018
VL - 320
JO - Ocean Engineering
JF - Ocean Engineering
M1 - 120371
ER -