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个人简介

招生方向 航空发动机气动热力学 叶轮机械高精度测试技术 教育背景 2007-09--2010-06 加拿大 Carleton 大学 联合培养博士 2005-09--2010-07 西北工业大学 博士 2001-09--2005-07 西北工业大学 学士 工作简历 2012-07~2014-06,加拿大 National Research Council Canada, Research Associate 2010-07~2012-06,加拿大 National Research Council Canada, Research Assistant 奖励信息 (1) 中国科学院“****”终期优秀奖, 院级, 2019 (2) 先进轻型航空动力研究集体, , 部委级, 2018 (3) 新型布局斜流离心组合压气机设计方法, 二等奖, 部委级, 2016 专利成果 ( 1 ) 一种具有马蹄形扩压通道的叶片式扩压器 , 发明, 2013, 第 2 作者, 专利号: 201310714361.8 ( 2 ) 一种高低压涡轮的过渡段结构, 实用新型, 2014, 第 2 作者, 专利号: 201320558177.4 ( 3 ) 一种高低压涡轮过渡段布局结构及设计方法, 发明, 2015, 第 2 作者, 专利号: 201410004116.2 ( 4 ) 一种高低压涡轮的过渡段结构, 发明, 2013, 第 2 作者, 专利号: 201310407137.4 ( 5 ) 一种离心压气机径向扩压器试验装置及其试验方法, 发明, 2014, 第 2 作者, 专利号: 201410645069.X ( 6 ) 一种具有径向分叉叶片的风扇整流器及其设计方法, 发明, 2013, 第 2 作者, 专利号: 201310596821.1 ( 7 ) 超高负荷低压涡轮叶片、高负荷低压涡轮、航空燃气涡轮发动机, 发明, 2015, 第 1 作者, 专利号: 201510169276.7 ( 8 ) 一种具有扩张型子午流道的轴流压气机及其设计方法, 发明, 2013, 第 2 作者, 专利号: 201310575261.1 ( 9 ) 一种具有顶部开叉的压气机转子叶片及设计方法, 发明, 2013, 第 3 作者, 专利号: 201410169055.5 ( 10 ) 整流器、流道结构、组合压气机、航空燃气涡轮发动机, 发明, 2018, 第 2 作者, 专利号: 201510219746.6 ( 11 ) 压气机或涡轮出口导向器, 发明, 2019, 第 1 作者, 专利号: 201510882628.3 ( 12 ) 用于航空燃气涡轮发动机的大攻角包容性涡轮叶片, 发明, 2017, 第 1 作者, 专利号: 201610421643.2 ( 14 ) 一种超紧凑高掺混效率消旋波瓣混合排气系统结构, 发明, 2017, 第 3 作者, 专利号: 201610626733.5 ( 15 ) 一种适合航空发动机强剪切非定常流测试的探针组件, 发明, 2019, 第 1 作者, 专利号: 201611010275.9 ( 16 ) 一种冷却通道、冷却通道组及应用其的涡轮叶片, 发明, 2018, 第 3 作者, 专利号: 201710144157.5 ( 18 ) 一种轴流‑离心整体叶盘式组合压缩系统, 发明, 2018, 第 4 作者, 专利号: 201710286250.X ( 20 ) 一种蒸发管燃烧室用燃油喷射装置, 发明, 2018, 第 5 作者, 专利号: 201710286263.7 ( 21 ) 等离子体喷嘴, 发明, 2017, 第 5 作者, 专利号: 201710597633.9 ( 22 ) 燃烧器, 发明, 2017, 第 5 作者, 专利号: 201710597535.5 ( 23 ) 一种适合航空发动机强剪切非定常流的测试系统, 发明, 2018, 第 1 作者, 专利号: 201611010173.7 ( 24 ) 一种跨音速风扇叶顶基元叶型的削尖前缘结构及设计方法, 发明, 2018, 第 5 作者, 专利号: 201711003800.9 ( 25 ) 一种波瓣混合器的参数化设计方法, 发明, 2018, 第 3 作者, 专利号: 201710675738.1 ( 26 ) 一种发动机扭矩测量装置, 发明, 2017, 第 4 作者, 专利号: 201710009338.7 ( 27 ) 一种防止离心叶轮刮蹭的机匣波纹结构, 发明, 2018, 第 5 作者, 专利号: 201810509619.3 ( 28 ) 一种三维振动模态可调的叶片激振器及其设计方法, 发明, 2019, 第 2 作者, 专利号: 201810319544.2 参与会议 (1)Influence of the Sealing Efficiency and Loss Generation for Rim Seal under Variable Mainstream Incidence 2019-11-22 (2)Design and Test of a Novel Highly-Loaded Compressor 2019-06-17 (3)Study of Geometric Parameter Influence on Fishtail Pipe Diffuser Performance 2016-06-15 (4)Effects of Area Ratio and Mean Rise Angle on the Aerodynamics of Inter-Turbine Ducts Yanfeng Zhang, Shuzhen Hu, Ali Mahallati and Xue-Feng Zhang 2014-06-18 (5)Experimental and Numerical Investigation of Corner Stall in a Highly-Loaded Compressor Cascade Yanfeng Zhang, Ali Mahallati and Michael Benner 2014-06-16 (6)Aerodynamic Design of Low Aspect Ratio Structual Airfoils within an Inter-Turbine Duct Yanfeng Zhang, Xue Feng Zhang, Ali Mahallati and Edward Vlasic 2013-10-11 (7)Flow Control in an Aggressive Inter-Turbine Duct Using Low Profile Vortex Generators Yanfeng Zhang, Shuzhen Hu , Xue Feng Zhang, Michael Benner 2012-06-15 (8)Influence of Inlet Swirl Distributions on an Inter-Turbine Duct- Part II: Hub Swirl Variation Yanfeng Zhang, Shuzhen Hu , Xue Feng Zhang,Edward Vlasic 2011-06-09

研究领域

航空发动机气动热力学

近期论文

查看导师新发文章 (温馨提示:请注意重名现象,建议点开原文通过作者单位确认)

(1) Numerical simulations of flutter mechanism for high-speed wide-chord transonic fan, Aerospace Science and Technology, 2020, 通讯作者 (2) Effects of unsteady interaction on the performance of an ultra-high-pressure-ratio centrifugal compressor, Aerospace Science and Technology, 2020, 通讯作者 (3) Unsteady Experimental and Numerical Investigation of Aerodynamic Performance in Ultra-high-lift LPT, Chinese Journal of Aeronautics, 2020, 通讯作者 (4) Flow Mechanism Between Purge Flow and Mainstream in different Turbine Rim Seal Configurations, Chinese Journal of Aeronautics, 2020, 通讯作者 (5) Large Eddy Simulation of the Separated Flow Transition on the Suction Surface of a High Subsonic Compressor Airfoil, Physics of Fluids, 2020, 第 5 作者 (6) Unsteady Wakes–Secondary Flow Interactions in a High-Lift LPT Cascade, Chinese Journal of Aeronautics, 2020, 通讯作者 (7) Numerical simulations of flutter mechanism for high-speed wide-chord transonic fan, Aerospace Science and Technology, 2020, 通讯作者 (8) The Effect of Endwall Boundary Layer and Incoming Wakes on Secondary Flow in a High-Lift LPT Cascade at Low Reynolds Number, Proc IMechE Part G: Journal of Aerospace Engineering, 2019, 通讯作者 (9) Unsteady influences of blade loading distribution on secondary flow of ultra-high-lift LPT, Aerospace Science and Technology, 2019, 通讯作者 (10) Unsteady effects of periodic wake passing frequency on aerodynamic performance of ultra-high-lift low pressure turbine cascades, Physics of Fluids, 2019, 通讯作者 (11) Effects of a slotted diffuser on the aerodynamic performance of a highly loaded centrifugal compressor, Proc IMechE Part C: J Mechanical Engineering Science, 2019, 通讯作者 (12) Flow control of hub corner stall in a highly loaded axial compressor cascade, International Journal of Heat and Fluid Flow, 2019, 通讯作者 (13) Effect of Periodic Wakes and a Contoured Endwall on Secondary Flow in a High-Lift Low-Pressure Turbine Cascade at Low Reynolds Numbers, Computers and Fluids, 2019, 通讯作者 (14) Numerical Investigation of a HighlyLoaded Centrifugal Compressor Stage with a Tandem Bladed Impeller, Proc. IMechE Part A: Journal of Power and Energy, 2018, 通讯作者 (15) Investigation of two pipe diffuser configurations for a compact centrifugal compressor, Proc. IMechE Part G: Journal of Aerospace Engineering, 2018, 第 3 作者 (16) Effects of Area Ratio and Mean Rise Angle on the Aerodynamics of Interturbine Ducts, ASME Journal of Turbomachinery, 2018, 第 1 作者 (17) Effects of periodic wakes on the endwall secondary flow in high-lift low-pressure turbine cascades at low Reynolds numbers, Proc. IMechE Part G: Journal of Aerospace Engineering., 2017, 通讯作者 (18) Effects of Periodic Wakes on Boundary Layer Development on an Ultra-high-lift Low Pressure Turbine Airfoil, Proc. IMechE Part A: Journal of Power and Energy, 2017, 通讯作者 (19) Investigation of a high pressure ratio centrifugal compressor with wedge diffuser and pipe diffuser, International Journal of Turbo & Jet-Engine, 2017, 第 4 作者 (20) 高负荷低压涡轮内部非定常流动机理及其控制策略研究进展, 推进技术, 2017, 第 3 作者 (21) 几何参数对紧凑涡轮过渡段内部流动机理影响研究, 工程热物理学报, 2017, 第 1 作者 (22) 高压比离心压气机串列叶轮内部流动机理研究, 推进技术, 2017, 第 3 作者 (23) Numerical Research on the Mixing Mechanism of Lobed Mixer with New De-swirling Structure, ASME Paper, GT2016-58120, 2016, 第 2 作者 (24) Study of Geometric Parameter Influence on Fishtail Pipe Diffuser Performance, ASME Paper, GT2016-57404, 2016, 第 3 作者 (25) Parametric Studying of Low Profile Vortex Generators Flow Control in an Aggressive Inter-Turbine Duct, Proc. IMechE, Part A: Journal of Power and Energy., 2015, 第 1 作者 (26) Numerical Research on the Mixing Mechanism of Lobed Mixer with Inlet Swirl in Linear Radial Distribution, Proc. IMechE, Part A: Journal of Power and Energy., 2015, 通讯作者 (27) Flow Control in an Aggressive Inter-Turbine Duct Using Low Profile Vortex Generators, ASME Journal of Engineering for Gas Turbines and Power, 2014, 第 1 作者 (28) Experimental and Numerical Investigation of Corner Stall in a Highly-Loaded Compressor Cascade, ASME paper GT2014-27204, also accepted by ASME Journal of Turbomachinery, 2014, 第 1 作者 (29) Effects of Area Ratio and Mean Rise Angle on the Aerodynamics of Inter-Turbine Ducts, ASME paper GT2014-27207, also accepted by ASME Journal of Turbomachinery, 2014, 第 1 作者 (30) Aerodynamic Design of Low Aspect Ratio Structual Airfoils within an Inter-Turbine Duct, ISABE paper,2013-1149, 2013, 第 1 作者 (31) Flow Control in an Aggressive Inter-Turbine Duct Using Low Profile Vortex Generators, ASME Paper, GT2012-69951, 2012, 第 1 作者 (32) Influnence of Inlet Swirl Distributions on an Inter-Turbine Duct- Part I I: Hub Swirl Variation, ASME Paper, GT2011-45555, 2011, 第 1 作者 (33) Influnence of Inlet Swirl Distributions on an Inter-Turbine Duct-Part I: Casing Swirl Variation, ASME Paper, GT2011-45554, 2011, 第 2 作者 (34) Effects of Inlet Flow Conditions on the S-shape Inter-Turbine Duct, ISABE paper,2011-1711, 2011, 第 2 作者

学术兼职

2016-01-01-2020-12-31,中国空气动力学会计算空气动力学专业委员会, 专委会委员

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