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Li Yan

ocean university of china

45H指数
103论文数
5.6K被引数
收录论文 83
发表时间
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Numerical simulation of the aerodynamic characteristics of an HAWT with a circular hole at the blade tip带有圆形孔的HAWT叶片尖端的气动特性数值模拟
errJournal of Ocean Engineering and Science
IF11.8
err2025-10-10
err0
errOAAI
errShengbing Yang; Zhiyuan Liu; Yan Li
err分享
err收藏
Numerical study on the heat recovery of fractured rock under thermal-hydraulic coupling热-水力耦合作用下裂隙岩石热回收的数值研究
errInternational Journal of Heat and Mass Transfer
IF5.8
err2025-08-30
err0
PREAI
errAsif Mehmood; Zheng Chen; Atif Zafar; Chuan-Yong Zhu; Tao Zhang; Liang Gong; Yan Li
err分享
err收藏
Influences of microjet pressure and number of microjets on the control of shock wave/boundary layer interaction
errAEROSPACE SCIENCE AND TECHNOLOGY
IF5.8
err2023-07-01
err7
PREAI
errXu, Hao; Huang, Wei; Du, Zhao-bo; Meng, Yu-shan; Liu, Chao-yang; Yan, Li
err分享
err收藏
Effects of blade airfoil chord length and rotor diameter on aerodynamic performance of straight-bladed vertical axis wind turbines by numerical simulation
errENERGY
IF9.4
err2023-02-01
err35
PREAI
errTong, Guoqiang; Li, Yan; Tagawa, Kotaro; Feng, Fang
err分享
err收藏
Control of shock wave/boundary layer interaction induced by the microjet configuration
errACTA ASTRONAUTICA
IF3.4
err2022-12-01
err9
PREAI
errXu, Hao; Huang, Wei; Yan, Li; Du, Zhao-bo
err分享
err收藏
Control mechanism of micro vortex generator and secondary recirculation jet combination in the shock wave/boundary layer interaction
errACTA ASTRONAUTICA
IF3.4
err2022-11-01
err11
PREAI
errWu, Han; Huang, Wei; Yan, Li; Du, Zhao-bo
err分享
err收藏
Investigation on the adaptive control of shock wave/turbulent boundary layer interaction based on the secondary circulation jets
errACTA ASTRONAUTICA
IF3.4
err2022-09-01
err25
PREAI
errZhong, Xiang-yu; Huang, Wei; Yan, Li; Wu, Han; Du, Zhao-bo
err分享
err收藏
Drag and heat reduction mechanism induced by jet interaction over a reusable launch vehicle in hypersonic flows在高超声速流动中，可重复使用的运载火箭上的射流相互作用引起的阻力和热量减少机制
errACTA ASTRONAUTICA
IF3.4
err2022-09-01
err13
PREAI
errMeng, Yu-shan; Wang, Zhong-wei; Shen, Yang; Huang, Wei; Niu, Yao-bin; Yan, Li
err分享
err收藏
Design exploration on the drag reduction and thermal protection over a blunted waverider with multiple opposing jets具有多个相对射流的钝乘波体的减阻和热保护设计探索
errAEROSPACE SCIENCE AND TECHNOLOGY
IF5.8
err2022-05-01
err15
PREAI
errJi, Chen; Liu, Bing; Huang, Wei; Li, Shi-bin; Meng, Zhao-E; Yan, Li; Choubey, Gautam
err分享
err收藏
Investigation on the drag reduction and thermal protection properties of the porous opposing jet in the supersonic flow: A parametric study with constant mass flow rate
errAEROSPACE SCIENCE AND TECHNOLOGY
IF5.8
err2021-11-01
err20
PREAI
errJi, Chen; Liu, Bing; Huang, Wei; Li, Shi-bin; Yan, Li
err分享
err收藏
Parametric investigation on drag reduction and thermal protection characteristics of the porous opposing jet in the hypersonic flow高超声速流动中多孔相对射流的减阻和热防护特性的参数研究
errAEROSPACE SCIENCE AND TECHNOLOGY
IF5.8
err2021-09-01
err28
PREAI
errJi, Chen; Liu, Bing; Li, Shi-bin; Huang, Wei; Yan, Li
err分享
err收藏
Fluid-thermal coupled investigation on the combinational spike and opposing/lateral jet in hypersonic flows
errACTA ASTRONAUTICA
IF3.4
err2021-08-01
err23
PREAI
errMeng, Yu-shan; Yan, Li; Huang, Wei; Wang, Zhong-wei
err分享
err收藏
Coupled investigation on drag reduction and thermal protection mechanism of a double-cone missile by the combined spike and multi-jet
errAEROSPACE SCIENCE AND TECHNOLOGY
IF5.8
err2021-08-01
err35
PREAI
errMeng, Yu-shan; Yan, Li; Huang, Wei; Ji, Chen; Li, Jie
err分享
err收藏
Coupled investigation on drag and heat flux reduction over spiked waverider with a wide-speed range
errACTA ASTRONAUTICA
IF3.4
err2021-05-01
err17
PREAI
errMeng, Yu-shan; Yan, Li; Huang, Wei; Zhao, Zhen-tao
err分享
err收藏
Design exploration on the shock wave/turbulence boundary layer control induced by the secondary recirculation jet二次再循环射流引起的休克波/湍流边界层控制的设计探索
errACTA ASTRONAUTICA
IF3.4
err2021-04-01
err31
PREAI
errDu, Zhao-bo; Shen, Chi-bing; Shen, Yang; Huang, Wei; Yan, Li
err分享
err收藏
Design exploration on the mixing augmentation induced by the oblique shock wave and a novel step in a supersonic flow倾斜休克波和超音速流中新台阶引起的混合增强的设计探索
errACTA ASTRONAUTICA
IF3.4
err2021-03-01
err24
PREAI
errHuang, Wei; Wu, Han; Du, Zhao-bo; Yan, Li; Choubey, Gautam
err分享
err收藏
Parameterized modeling and optimization of reusable launch vehicles based on reverse design approach基于逆向设计方法的可重复使用运载火箭参数化建模与优化
errACTA ASTRONAUTICA
IF3.4
err2021-01-01
err15
PREAI
errLeng, Jun-xue; Shen, Yang; Zhang, Tian-tian; Huang, Wei; Yan, Li
err分享
err收藏
Parametric study on mixing augmentation mechanism induced by cantilevered ramp injectors in a shock-induced combustion ramjet engine
errAEROSPACE SCIENCE AND TECHNOLOGY
IF5.8
err2021-01-01
err43
PREAI
errDu, Zhao-bo; Shen, Chi-bing; Huang, Wei; Yan, Li; Liang, Jian-han; Choubey, Gautam
err分享
err收藏
Investigation on the mode transition of a typical three-dimensional scramjet combustor equipped with a strut
errENERGY
IF9.4
err2020-10-01
err24
PREAI
errYan, Li; Liao, Lei; Meng, Yu-shan; Li, Shi-bin; Huang, Wei
err分享
err收藏
Mixing and combustion in supersonic/hypersonic flows
errzhejiang university science b
IF3.9
err2020-09-30
err4
errOAAI
errHuang, Wei; Chang, Jun-tao; Yan, Li
err分享
err收藏

研究方向

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合作学者
合作期刊
张涛 封面图
张涛 (Tao Zhang)
H 指数: 67 · 论文数: 848
W
Wei Huang
H 指数: 61 · 论文数: 357
刘
刘卫东 (Weidong Liu)
H 指数: 58 · 论文数: 714
Z
Zheng Chen
H 指数: 51 · 论文数: 314
陈政 封面图
陈政 (Zheng Chen)
H 指数: 51 · 论文数: 287
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