VANE

作品数:105被引量:250H指数:8
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相关作者:李世林张宇魏强陈丽华浦仁旺更多>>
相关机构:中国民用航空飞行学院大连医科大学附属第一医院西北工业大学南京航空航天大学更多>>
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3D Vane序列结合膈肌导航技术在肝脏TIWI中应用的可行性探讨
《中国CT和MRI杂志》2025年第1期109-111,共3页穆晶 袁颖 
国家自然科学基金项目(52227814);国家自然科学基金面上项目(批准号82371904)。
目的 对比分析常规肝脏T1WI快速成像屏气检查3D mDixon序列与应用膈肌导航技术在自由呼吸下采集的3D Vane序列的图像质量,探讨膈肌导航技术结合3D Vane序列自由呼吸下扫描肝脏T1WI检查中的可行性。方法 选取2023年3月至10月期间的70名肝...
关键词:膈肌导航技术 3D VANE 自由呼吸 肝脏T1WI 
Flow Analysis of Tandem Blades as the Outlet Vane of a Highly Loaded Compressor
《Journal of Thermal Science》2024年第6期2005-2018,共14页LUO Qiao LUO Lei DU Wei YAN Han WANG Songtao ZHOU Xun 
supported by the National Science and Technology Major Project (Nos.2017-Ⅱ-0007-0021 and P2021-AB-I-003-001);the Heilongjiang Province Postdoctoral Special Funding (LBH-TZ2109)
A tandem blade configuration is a significant flow control method that delays the onset of flow separation.This study numerically investigates the effects of diffusion factor and percentage pitch on the flow structure...
关键词:COMPRESSOR tandem blade loss corner separation gap flow 
Turbine Passage Secondary Flow Dynamics and Endwall Heat Transfer Under Different Inflow Turbulence
《Journal of Harbin Institute of Technology(New Series)》2024年第3期51-62,共12页Arjun K S Tide P S Biju N 
This study presents endwall hydrodynamics and heat transfer in a linear turbine cascade at Re 5×105 at low and high intensities of turbulence.Results are numerically predicted using the standard SST model and Reθ-γ...
关键词:TURBINE VANE heat transfer ENDWALL TURBULENCE secondary flow 
Optimum Profiles of Endwall Contouring for Enhanced Net Heat Flux Reduction and Aerodynamic Performance被引量:1
《Journal of Harbin Institute of Technology(New Series)》2024年第2期80-92,共13页Arjun K S Tide P S Biju N 
Successfully utilized non-axisymmetric endwalls to enhance turbine efficiencies(aerodynamic and turbine inlet temperatures)by controlling the characteristics of the secondary flow in a blade passage.This is accomplish...
关键词:endwall contouring turbine VANE heat transfer phantom cooling coolant injection net heat flux reduction aerodynamic performance 
船体风机叶片对中速船水动力性能影响的计算分析被引量:1
《哈尔滨工程大学学报(英文版)》2023年第4期762-774,共13页S.Gopinath R.Vijayakumar 
The importance of reducing ship resistance is growing considerably as a result of the increase in atmospheric emissions and the drive towards green shipping through decarbonization.Until this point,Energy Saving Devic...
关键词:Decarbonization Green shipping Ship resistance Energy saving devices(ESD) Hull vane®.(HV) Angle of foil(AoF) 
3D Vane⁃XD⁃mDixon序列在胸椎增强MRI中的应用效果评价被引量:1
《岭南现代临床外科》2023年第5期405-409,共5页谢定祥 陈笑芳 张印宏 吴嘉乐 马慧 蔡华崧 张馨月 
国家自然科学基金青年基金(82202217)。
目的探究3D⁃VANE⁃XD⁃mDixon序列在胸椎增强核磁共振成像(MRI)成像中对图像质量的影响及其应用价值。方法收集临床怀疑胸椎病变患者63例,行常规胸椎MRI后补充3D⁃T1WI⁃mDixon⁃TSE及3D⁃Vane⁃XD⁃mDixon序列。计算并测量两种扫描序列图像的...
关键词:胸椎 磁共振成像 3D⁃Vane⁃XD⁃mDixon序列 
Numerical and experimental study on the particle erosion and gas–particle hydrodynamics in an integral multi-jet swirling spout-fluidized bed
《Chinese Journal of Chemical Engineering》2023年第9期90-101,共12页Wenbin Li Feng Wu Liuyun Xu Jipeng Sun Xiaoxun Ma 
supported by the National Natural Science Foundation of China(22178286);Shaanxi Qin Chuangyuan“scientist and engineer”team construction project(2022KXJ-041)。
In this paper,using the computational fluid dynamics based on Euler Lagrange and the commercial software Barracuda VR,the gas-particle hydrodynamics and the erosion of particles on the inner wall and internal componen...
关键词:Integral multi-jet swirling spout-fluidized bed Gas–particle hydrodynamics Axial swirl vane Uneven Erosion 
Understanding of tip clearance flow structure in high speed mixed flow compressor
《Propulsion and Power Research》2023年第3期356-379,共24页Hemant Kumar Chetan S.Mistry 
This paper addresses the necessity to make a physical interpretation of a highly complex three-dimensional tip clearance flow field study for high-speed mixed-flow compressor having stage exit static pressure to inlet...
关键词:Recirculation zone Vortex breakdown Tip leakage flow Mixed-flow compressor Jet-wake flow Vaned-diffuser 
Design Optimization of Non-Axisymmetric Vane for an Axial Compressor under Inlet Distortion被引量:3
《Journal of Thermal Science》2023年第4期1321-1334,共14页ZHANG Min DU Juan ZHAO Hongliang QIU Jiahui BA Dun CHEN Yang NIE Chaoqun 
The authors gratefully acknowledge the support of the National Science and Technology Major Project(J2019-II-0017-0038);the National Natural Science Foundation of China(NSFC 52206061);Science Center for Gas Turbine Project(P2022-A-II-002-001).
The flow field at the inlet of compressors is generally encountered combined total pressure and swirl distortion for either aircraft engine with S-duct or gas turbine with lateral air intake.This inevitably deteriorat...
关键词:combined total pressure and swirl distortion axial compressor non-axisymmetric vane OPTIMIZATION aerodynamic performance 
Numerical Investigation of Flow and Heat Transfer in Vane Impingement/Effusion Cooling with Various Rib/Dimple Structure被引量:1
《Journal of Thermal Science》2023年第4期1357-1377,共21页WANG Mingrui ZHU Huiren LIU Cunliang WANG Rui WU Zhuang YAO Chunyi 
This study is financially supported by the National Science and Technology Major Project(2017-III-0003-0027).
By investigating heat transfer and flow structures of dimples,orthogonal ribs,and V-shaped ribs in the impingement/effusion cooling,the article is dedicated to selecting a best-performing internal cooling structure fo...
关键词:conjugate heat transfer impingement cooling DIMPLE V-shape rib discharge coefficient 
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