云南高校图书馆联盟文献共享服务平台- EXIT

EXIT: 作品数：192被引量：259H指数：8; 导出分析报告; 相关领域：电子电信更多>>; 相关作者：陶国才张铭毕敏吴艳顾健腾更多>>; 相关机构：北京邮电大学第三军医大学西南医院复旦大学云南财经大学更多>>; 相关期刊：更多>>; 相关基金：国家自然科学基金国家重点基础研究发展计划中国博士后科学基金国家高技术研究发展计划更多>>

Design Optimization and Analysis of Exit Rotor with Diffuser Passage based on Neural Network Surrogate Model and Entropy Generation Method被引量：1: 《Journal of Thermal Science》2023年第2期739-752,共14页JIN Yun GENG Shaojuan LIU Shuaipeng NI Ming ZHANG Hongwu; the support of the National Science and Technology Major Project(2017-Ⅱ-0006-0020)。; In this paper,a diffuser passage compressor design is introduced via optimization to improve the aerodynamic performance of the exit rotor in a multistage axial compressor.An in-house design optimization platform,base...; 关键词：exit rotor diffuser passage neural network surrogate model entropy generation rate flow blockage

Influence of Turbulence Schmidt Number on Exit Temperature Distribution of an Annular Gas Turbine Combustor using Flamelet Generated Manifold被引量：1: 《Journal of Thermal Science》2020年第1期58-68,共11页WANG Weihao YANG Songlin GAO Chuang HUANG Weiguang; funded by the Key Programs of Chinese Academy of Sciences (Project No. ZDRW-CN-2017-2); The Reynolds analogy concept has been used in almost all turbulent reacting flow RANS(Reynoldsaveraged Navier–Stokes)simulations,where the turbulence scalar transfers in flow fields are calculated based on the modele...; 关键词：gas turbine combustor flamelet-generated manifold turbulent Schmidt Number Reynolds Stress Model Reynolds analogy

Simulation of a Shock Tube with a Small Exit Nozzle: 《Journal of Thermal Science》2018年第1期34-38,共5页Yigang Luan Matthias Olzmann Franco Magagnato; supported by the DFG(Deutsche Forschungsgemeinschaft)[SFB-TRR 150“Turbulent,Chemically Reactive Multi-Phase Flows near Walls”,sub-projects B02 and B04]; Shock tubes are frequently used to rapidly heat up reaction mixtures to study chemical reaction mechanisms and kinetics in the field of combustion chemistry [1]. In the present work, the flow field inside a shock tube...; 关键词：CFD shock tube low pressure numerical scheme

Numerical Study of Effect of Compressor Swirling Flow on Combustor Design in a MTE被引量：3: 《Journal of Thermal Science》2017年第4期349-354,共6页MU Yong WANG Chengdong LIU Cunxi LIU Fuqiang HU Chunyan XU Gang ZHU Junqiang; supported by National Natural Science Foundation of China with project No.51406202; An effect of the swirling flow on the combustion performance is studied by the computational fluid dynamics(CFD) in a micro-gas turbine with a centrifugal compressor, dump diffuser and forward-flow combustor. The dist...; 关键词：COMBUSTOR CFD Compressor exit flow angle Micro Turbojet Engine （MTE）

Temperature and Pressure Measurements at Cold Exit of Counter-flow Vortex Tube with Flow Visualization of Reversed Flow: 《Journal of Thermal Science》2015年第1期67-72,共6页Mohd Hazwan bin Yusof Hiroshi Katanoda Hiromitsu Morita; In order to clarify the structure of the cold flow discharged from the counter-flow vortex tube(VT), the temperature and pressure of the cold flow were measured, and the existence and behavior of the reversed flow at ...; 关键词：Vortex tube Reversed flow Flow visualization Pressure measurement Temperature measurement

Experimental Study of Effects of One Kind of Tangentially Non-uniform Tip Clearance on the Flow Field at an Exit of a Compressor Cascade Passage被引量：3: 《Journal of Thermal Science》2010年第1期7-13,共7页Hongwei MA Jinghui ZHANG Jun ZHANG; funded by the National Natural Science Foundation of China, Grant No 50776004;supported by the 111 Project, No B07009;973 Project, No 2007CB210103; This paper presents an experimental investigation of effects of one kind of tangentially non-uniform tip clearance on the flow field at an exit of a compressor cascade passage.The tests were performed in a low-speed l...; 关键词：compressor cascade CLEARANCE leakage flow secondary flow vortex

Numerical Simulation of High-Power Synthetic Jet Actuator Flowfield and its Influence on Mixing Control被引量：1: 《Journal of Thermal Science》2008年第3期207-211,共5页Yanming LIU Baoguo WANG Shuyan LIU; Postdoctoral Science Foundation of China,Grant No.20070420300; Detailed two-dimensional unsteady numerical simulation is carried out to investigate a high-power synthetic jet actuator flow field and its design characteristic. Simultaneously, mixing control mechanism of coaxial je...; 关键词：High-power synthetic jet actuator Mixing control Exit velocity Mixing enhancement

Effects of a Kind of Non-smooth Blade on the Unsteady Flow Field at the Exit of an Axial Fan: 《Journal of Thermal Science》2008年第1期1-6,共6页Hongwei MA Jibo GUO; National Natural Science Foundation of China,Grant No.50376002;the 111 Project,No.B07009; An experimental investigation of effects of a kind of streamwise-grooved blade on the unsteady flow field at an exit of an axial-flow fan was performed. The flow field at 25% chord downstream from the trailing edge at...; 关键词：axial fan non-smooth blade stream-wise groove unsteady flow.

Control of Collection Efficiency for Axial Flow Cyclone Dust Collectors with Fixed Guide Vanes and with Funnel Shaped Exit Pipes被引量：4: 《Journal of Thermal Science》2006年第3期240-250,共11页Akira Ogawa Masaru Arakawa; The experimental result of the collection efficiency of the axial flow cyclone with the fixed guide vanes is lower than that with the tangential inlet pipe to the cyclone body due to the weak angular momentum transfer...; 关键词：Axial flow cyclone funnel shaped exit pipe fixed guide vanes pressure drop collection efficiency Froude number cut-Size

Effect of Exit Geometry of Tail Pipe on the Performance of Pulse Jet Engines: 《Journal of Thermal Science》2006年第3期263-268,共6页Toshihiro NAKANO ShigeruMATSUO KenbuTERAMOTO ToshiakiSETOGUCHI; In this paper,the effect of geometries of tube open end on the shock,compression and expansion wavespropagating in the tube was investigated numerically and experimentally.One of them is a conventional straightshock t...; 关键词：compressible flow shock wave expansion wave pulse jet numerical simulation

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