Coupled response of flow-induced vibration and flow-induced rotation of a circular cylinder with a triangular fairing DOI
Hongjun Zhu, Hongtao Hao, Bin Liu

и другие.

Physics of Fluids, Год журнала: 2024, Номер 36(7)

Опубликована: Июль 1, 2024

In this paper, a numerical simulation investigation is carried out on the coupled response of flow-induced vibration (FIV) and rotation (FIR) circular cylinder attached with triangular fairing at low Reynolds number Re = 100. The primary focus impact FIR FIV. response, hydrodynamic coefficient, vortex shedding mode, flow field characteristics are examined for fairings within vibrational reduced velocity Ur range 3–16 shape angle α 45°, 60°, 90°. results reveal that Ur, all three considered have good suppression effect Nevertheless, galloping emerges as increases when 45° 60°. contrast, 90° presents wider lock-in region. rotatable 2-degree freedom (2-DoF) has better performance in reduction amplitude coefficients. 2S (two single vortices) mode mainly occurs vortex-induced (VIV) region, while 2S–8S (from two to eight vortices), 2P pairs 2T triplets P + T (a pair vortices triple modes emerge branch. Moreover, four wake structures identified according variation recirculation region migration boundary layer separation point. Finally, regions drag, lift, highlighted compared bare cylinder.

Язык: Английский

Forced vibration analysis of a spinning Timoshenko beam under axial loads by means of the 3-dimensional Green’s functions DOI
Long Wang,

Mingze Yuan,

Xiangyong Zhao

и другие.

International Journal of Solids and Structures, Год журнала: 2025, Номер unknown, С. 113324 - 113324

Опубликована: Март 1, 2025

Язык: Английский

Процитировано

0

Sampled-data fuzzy modeling and control for offshore structures subject to parametric perturbations and wave loads DOI
Zhihui Cai, Bao‐Lin Zhang, Qing‐Long Han

и другие.

Ocean Engineering, Год журнала: 2025, Номер 326, С. 120908 - 120908

Опубликована: Март 12, 2025

Язык: Английский

Процитировано

0

Passive control of rotational response of a square cylinder with small circular rods DOI
Tao Tang, Hongjun Zhu

Physics of Fluids, Год журнала: 2025, Номер 37(4)

Опубликована: Апрель 1, 2025

This work proposed a passive method by arranging several small circular rods to control the rotational dynamics of square cylinder. Two-dimensional numerical investigations were conducted at low Reynolds number 120 and in wide reduced velocity range Ur = 2–20. Effects rod arrangement as well gap distance between cylinder examined. For single cylinder, critical 6.5 is identified. Rotary angles remain near zero 2–6, while sharp rise occurs 6.5, reaching peak 38.05° 8, after which it slightly declines. The frequencies follow two different growth rates before velocity. When eight are evenly arranged around rotary structure do not exceed 5° 90% reductions achieved compared with showing most effective suppression. However, associated drag coefficients significantly increased due projected area in-line direction frequent separation reattachment behaviors. Optimal when placed windward leeward position, helpful reduce local high pressure recover base pressure, respectively. Bifurcation, characterized non-zero time-averaged angle, appears side-by-side position. After bifurcation, these stay below causing an asymmetrical configuration thus flow distributions. A recommended half length edge under across entire range, indicating perfectly excellent rotation At this configuration, no vortex shedding field stable symmetry.

Язык: Английский

Процитировано

0

Role of cross-flow vibrations in the flow-induced rotations of an elastically mounted cylinder-plate system DOI
Tao Tang, Hongjun Zhu, Qing Xiao

и другие.

Physics of Fluids, Год журнала: 2024, Номер 36(6)

Опубликована: Июнь 1, 2024

Vibration and rotation represent two common fluid–structure-interaction phenomena, which can occur independently or concurrently. While extensive research has been conducted on individual vibration/rotation cases, there is relatively limited literature coupled cases. However, it crucial to recognize that responses, such as those observed in falling leaves, are more prevalent both natural occurrences engineering scenarios. Hence, this study aims investigate the influence of cross-flow vibrations flow-induced rotations an elastically mounted cylinder-plate system. A broad range rotational reduced velocities, spanning Uθ = 2–18, examined across four distinct vibrational namely Uy 5, 8, 12, 18. Numerical results indicated a bifurcation phenomenon, wherein deflects non-zero equilibrium position, occurs at high values Uy. Four response modes have identified: vibration-dominated, rotation-dominated, augmentation (VIV-like), (galloping-like) mode. These exert significant phase angles between rotary angle displacement well vortex shedding modes. In rotation-dominated region, VIV-like galloping-like exhibit continuous decreasing trend, consistent level 180° 90°, respectively. Transitions vibration responses result sharp increases angles. The wake flow mode demonstrates 2S (two single vortices), while vibration-dominated characterized by predominant 2T triplets vortices). large amplitudes lead increase numbers vortices, presenting 2S, 2S*, 2P pairs vortices) 2P, P + S (one pair one 2P+S where 2S* consists each exhibiting tendency split into smaller vortices they migrate downward. mechanism behind notable amplification rotation/vibration elucidated. Apart from pressure difference induced shedding, additional driving force resulting relative motion transverse direction contributes total torsional force, thereby leading responses. Furthermore, streamlined profile accounts for escalation amplitudes.

Язык: Английский

Процитировано

1

Coupled response of flow-induced vibration and flow-induced rotation of a circular cylinder with a triangular fairing DOI
Hongjun Zhu, Hongtao Hao, Bin Liu

и другие.

Physics of Fluids, Год журнала: 2024, Номер 36(7)

Опубликована: Июль 1, 2024

In this paper, a numerical simulation investigation is carried out on the coupled response of flow-induced vibration (FIV) and rotation (FIR) circular cylinder attached with triangular fairing at low Reynolds number Re = 100. The primary focus impact FIR FIV. response, hydrodynamic coefficient, vortex shedding mode, flow field characteristics are examined for fairings within vibrational reduced velocity Ur range 3–16 shape angle α 45°, 60°, 90°. results reveal that Ur, all three considered have good suppression effect Nevertheless, galloping emerges as increases when 45° 60°. contrast, 90° presents wider lock-in region. rotatable 2-degree freedom (2-DoF) has better performance in reduction amplitude coefficients. 2S (two single vortices) mode mainly occurs vortex-induced (VIV) region, while 2S–8S (from two to eight vortices), 2P pairs 2T triplets P + T (a pair vortices triple modes emerge branch. Moreover, four wake structures identified according variation recirculation region migration boundary layer separation point. Finally, regions drag, lift, highlighted compared bare cylinder.

Язык: Английский

Процитировано

1