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Quanyong Xu
tsinghua university
10
H指数
42
论文数
250
被引数
0
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13
发表时间
发表时间
IF
被引数
Blade3DNO: Geometry-consistent spectral operator learning for transonic 3D compressor flows
Blade3DNO: 几何一致性谱算子学习用于跨声速三维压气机流场
Aerospace Science and Technology
IF
5.8
2026-04-13
0
PRE
AI
Liangrui Wei; Yuxin Zhao; Zhou Du; Quanyong Xu; Feng Zhou
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BladeNet3D: A high-fidelity structured CFD dataset and generation pipeline for data-driven design of transonic compressor blades
BladeNet3D:一个高保真度结构化CFD数据集和用于跨音速压气机叶片数据驱动设计的生成流水线
Aerospace Science and Technology
IF
5.8
2026-03-24
0
PRE
AI
Yuxin Zhao; Liangrui Wei; Quanyong Xu; Feng Zhou; Zhou Du
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收藏
Compressor aerodynamic design based on artificial intelligence: Literature review and future direction
基于人工智能的压缩机气动设计:文献综述与未来方向
Engineering Applications of Artificial Intelligence
IF
8
2026-03-07
0
PRE
AI
Quanyong Xu; Yanjie Li
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The impact of the combined total pressure-swirl distortion on a transonic compressor rotor
组合总压-旋流畸变对跨声速压气机转子的影响
Aerospace Science and Technology
IF
5.8
2025-07-07
0
PRE
AI
Quanyong Xu; Jie Wu; Honghu Wu
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Enhancing accuracy of one-dimensional characteristic predictions for axial compressors using deep learning
利用深度学习提升轴流压缩机一维特性预测的准确性
ENGINEERING APPLICATIONS OF ARTIFICIAL INTELLIGENCE
IF
8
2025-06-01
0
PRE
AI
Ma, Yulin; Du, Zhou; Xu, Quanyong
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收藏
Flow field reconstruction of compressor blade cascade based on deep learning methods
AEROSPACE SCIENCE AND TECHNOLOGY
IF
5.8
2024-12-01
5
PRE
AI
Ma, Yulin; Du, Zhou; Xu, Quanyong; Qi, Jiaheng
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Simulation of coupling characteristics of motion and heat transfer between airflow and ice crystals in a single-stage compressor
PROPULSION AND POWER RESEARCH
IF
6.3
2024-12-01
0
OA
AI
Huang, Ping; Bu, Xueqin; Lin, Guiping; Xu, Quanyong; Xiao, Chunhua
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Effects of rotor squealer tip with non-uniform heights on heat transfer characteristic and flow structure of turbine stage
PHYSICS OF FLUIDS
IF
4.3
2024-11-13
0
PRE
AI
Cheng, Hongzhi; Liang, Haoqian; Wang, Dong; Zhou, Shuyu; Xu, Quanyong; Zhu, Zihao; Duan, Penghao
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The icing characteristic of stage 35 compressor blades and its impact on aerodynamic performance
AEROSPACE SCIENCE AND TECHNOLOGY
IF
5.8
2024-07-01
1
PRE
AI
Wu, Jie; Xu, Quanyong; Wu, Feng; Xia, Quanzhong; Xu, Qiannan
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Aerothermal optimization of turbine cascade squealer tip with non-uniform squealer height
PHYSICS OF FLUIDS
IF
4.3
2023-11-01
12
PRE
AI
Cheng, Hongzhi; Shahid, Hanzla; Zhou, Shuyu; Wang, Wei; Xu, Quanyong; Duan, Penghao
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Pressure and velocity fluctuations characteristics of the tip clearance flow in an axial compressor stage at the near-stall condition
近失速条件下轴流压气机级叶尖间隙流的压力和速度波动特性
AEROSPACE SCIENCE AND TECHNOLOGY
IF
5.8
2022-10-01
12
PRE
AI
Xu, Quanyong; Wu, Jie; Wu, Lin; Yang, Hui; Wang, Zhengdao; Wei, Yikun
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Effect of swirl field on the fuel concentration distribution and combustion characteristics in gas turbine combustor with cavity
旋流场对空腔燃气轮机燃烧室燃料浓度分布及燃烧特性的影响
ENERGY
IF
9.4
2018-11-01
23
PRE
AI
Zhang, Rongchun; Xu, Quanyong; Fan, Weijun
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A new closed-form method for inertia force and moment calculation in reciprocating piston engine design
SCIENCE CHINA-TECHNOLOGICAL SCIENCES
IF
4.9
2018-01-24
5
PRE
AI
Xie ZhiFeng; Xu QuanYong; Guan NanXiang; Zhou Ming
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研究方向
暂时未获取到该数据
合作学者
合作期刊
武林
(Lin Wu)
H 指数: 46 · 论文数: 355
J
Jie Wu
H 指数: 38 · 论文数: 345
G
Guiping Lin
H 指数: 35 · 论文数: 392
Z
Zhengdao Wang
H 指数: 31 · 论文数: 219
P
Ping Huang
H 指数: 27 · 论文数: 132
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