Ling Wan

Prof. Dr. Ling Wan

Faculty of Maritime and Transportation, Ningbo University, Ningbo 315211, China
orcid

Research Focus & Metrics

Academic Career Length

10Years (2017-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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7 March 2024 in Energy
Verified
Journal Article
Closed access
Ling WanLing Wan
Ling Wan
TMTorgeir Moan
Torgeir Moan
ZGZhen Gao
Zhen Gao
WSWei Shi
Wei Shi

8 February 2023 in Ocean Engineering
Verified
Journal Article
Closed access
WTWeijun Tian
Weijun Tian
YWYapo Wang
Yapo Wang
Wei ShiWei Shi
Wei Shi
Constantine MichailidesConstantine Michailides
Constantine Michailides
Ling WanLing Wan
Ling Wan
MINGSHENG CHENMINGSHENG CHEN
MINGSHENG CHEN

1 July 2019 in Ocean Engineering
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Journal Article
Closed access
CZChi Zhang
Chi Zhang
Ling WanLing Wan
Ling Wan
AMAllan R. Magee
Allan R. Magee
MHMengmeng Han
Mengmeng Han
JJJingzhe Jin
Jingzhe Jin
ØHØyvind Hellan
Øyvind Hellan

14 July 2024 in Case Studies in Thermal Engineering
Verified
Journal Article
Open access
YLYafei Li
Yafei Li
FSFan Shi
Fan Shi
JXJianjian Xin
Jianjian Xin
LPLiang Peng
Liang Peng
Ling WanLing Wan
Ling Wan

1 November 2024 in Physics of Fluids
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Journal Article
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PDF file
FSFulong Shi
Fulong Shi
JXJianjian Xin
Jianjian Xin
QJQiu Jin
Qiu Jin
Yang YangYang Yang
Yang Yang
Ling WanLing Wan
Ling Wan
Fish in nature can encounter various flow environments. This paper numerically simulated a 3D (three-dimensional) carangiform fish swimming in oblique flow. The numerical model adopts a robust ghost cell method with graphics processing unit acceleration. The dynamic performance and the 3D wake evolutions are discussed under different Strouhal numbers and attack angles. It is found that the thrust along the swimming direction would get enhanced with more energy consumption as the Strouhal number (St) rises. The attack angle can get the similar but less significant effect. Also, the stall angle of θ = 40° is approximately determined, which is independent of the Strouhal number. However, the flexible deformation can reduce the adverse effects of the stall. In terms of the wake structures, they are transitioned from the two rows of vortex streets at St = 0.2 to the three rows at St = 0.6, and even to the four rows at St = 1. The connected oblique vortex ring rows induced by the undulating caudal fin contributes to the thrust and lateral forces dominantly. As the St rises, the vortex ring rows is transformed from the typical von Karman vortex streets to the reverse one, indicating the generation of thrust. The slender, parallel vortex contrails are caused by the detachment of leading-edge vortices (LEVs), and they induce the high-order harmonic components in force coefficients. The oblique angle of the vortex rings grows with the Strouhal number, while it is hardly affected by the attack angle. As the attack angle grows, the wake is turned from the disconnected hairpin vortices to the intertwined vortex rings and losses the spanwise symmetry. Moreover, the reattachment of the LEV is not observed after the stall angle.

Verified
Journal Article
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XCXing Chang
Xing Chang
Y1Yin Pandeng 1
Yin Pandeng 1
JXJianjian Xin
Jianjian Xin
FSFulong Shi
Fulong Shi
Ling WanLing Wan
Ling Wan
To clarify the hydrodynamic interference characteristics of flows around multiple cylinders under the wall effect, the two-dimensional (2D) flows around the near-wall single, two tandem and parallel cylinders are simulated under different gap ratios (0.15 ≤ G/D ≤ 3.0) and spacing ratios (1.5 ≤ T/D ≤ 4.0) at a Reynolds number of Re = 6300. We also examine the wake patterns, the force coefficients, and the vortex-shedding frequency with emphases on the wall effect and effects of the two-cylinder interference. A critical wall gap of G/D = 0.6 is identified in the single-cylinder case where the wall can exert significant influences. The two near-wall tandem cylinders exhibit three wake states: stretching mode, attachment mode, and impinging mode. The force coefficients on the upstream cylinder are significantly affected by the wall for G/D ≤ 0.6. The downstream cylinder is mainly influenced by the upstream cylinder. For G/D > 0.6, the force coefficients on the two cylinders exhibit a similar variation trend. In the parallel arrangement, the two cylinders exhibit four wake states in different G/D and T/D ranges: double stretching mode, hetero-vortex scale mode, unilateral vortex mode, and free vortex mode. Moreover, the two parallel cylinders in the hetero-vortex scale or free vortex mode have two states: synchronous in-phase state and synchronous out-of-phase state. The mean drag coefficients on the two cylinders decrease, while the mean lift coefficients exhibit opposite variation trends, as the T/D grows.