叶轮机械气动热力学

涡轴发动机总体

   

080701-工程热物理
080703-动力机械及工程
082502-航空宇航推进理论与工程

航空发动机气动热力学
涡轴发动机总体设计

2012-09--2015-06   中国科学院大学工程热物理研究所   研究生，工学博士
2008-09--2010-06   东北大学   研究生，工学硕士
2004-09--2008-06   沈阳航空航天大学   本科，工学学士

研究生

工学博士

   

2019-06~现在, 中国科学院工程热物理研究所, 副研究员
2015-07~2019-05,中国科学院工程热物理研究所, 助理研究员
2010-07~2012-08,中国航发湖南动力机械研究所, 设计员

流体动力学测试技术

   

（1） Design Optimization of a Multistage Axial Flow Compressor Based on Full-Blade Surface Parameterization and Phased Strategy, INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2021, 第 4 作者
（2） Investigation of a High Pressure Ratio Centrifugal Compressor with Wedge Diffuser and Pipe Diffuser, INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2021, 第 2 作者
（3） Effect of Non-Axisymmetric End Wall on a Highly Loaded Compressor Cascade in Multi-Conditions, Effect of Non-Axisymmetric End Wall on a Highly Loaded Compressor Cascade in Multi-Conditions, JOURNAL OF THERMAL SCIENCE, 2021, 通讯作者
（4） Numerical investigation of distributed roughness effects on separated flow transition over a highly loaded compressor blade, PHYSICS OF FLUIDS, 2021, 第 3 作者
（5） Effects of surface roughness on the aerodynamic performance of a high subsonic compressor airfoil at low Reynolds number, Effects of surface roughness on the aerodynamic performance of a high subsonic compressor airfoil at low Reynolds number, CHINESE JOURNAL OF AERONAUTICS, 2021, 第 2 作者
（6） A Phased Aerodynamic Optimization Method for Compressors Based on Multi-Degrees-of-Freedom Surface Parameterization, A Phased Aerodynamic Optimization Method for Compressors Based on Multi-Degrees-of-Freedom Surface Parameterization, JOURNAL OF THERMAL SCIENCE, 2021, 第 2 作者
（7） Large eddy simulation of the separated flow transition on the suction surface of a high subsonic compressor airfoil, PHYSICS OF FLUIDS, 2020, 第 3 作者
（8） Numerical investigations of the separated transitional flow over compressor blades with different loading distributions, AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 第 3 作者
（9） Optimization Design of a 2.5 Stage Highly Loaded Axial Compressor with a Bezier Surface Modeling Method, APPLIED SCIENCES-BASEL, 2020, 第 3 作者
（10） 静叶轮毂间隙对高负荷压气机性能的影响研究, Research on the Influence of Stator Hub Gap on the Performance of High-Load Compressor, 工程热物理学报, 2020, 第 2 作者
（11） 采用鲸鱼算法的可控扩散叶型优化设计, Optimal Design of a Controlled Diffusion Airfoil with the Whale Algorithm, 西安交通大学学报, 2020, 第 2 作者
（12） Numerical and experimental investigation of flow mechanism and application of tandem-impeller for centrifugal compressor, AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 第 5 作者
（13） Inducer/Exducer Matching Characteristics inside Tandem Impellers of a Highly Loaded Centrifugal Compressor, Inducer/Exducer Matching Characteristics inside Tandem Impellers of a Highly Loaded Centrifugal Compressor, JOURNAL OF THERMAL SCIENCE, 2020, 第 5 作者
（14） Multipoint design optimization for a controlled diffusion airfoil compressor cascade, PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART C-JOURNAL OF MECHANICAL ENGINEERING SCIENCE, 2020, 通讯作者
（15） Numerical investigation of flow mechanisms of tandem impeller inside a centrifugal compressor, Numerical investigation of flow mechanisms of tandem impeller inside a centrifugal compressor, CHINESE JOURNAL OF AERONAUTICS, 2019, 第 5 作者
（16） DESIGN AND TEST OF A NOVEL HIGHLY-LOADED COMPRESSOR, PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2019, VOL 2A, 2019, 通讯作者
（17） Numerical investigation of a highly loaded centrifugal compressor stage with a tandem bladed impeller, PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2018, 第 5 作者
（18） High-pressure ratio centrifugal compressor with two different fishtail pipe diffuser configurations, PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2018, 第 2 作者
（19） Investigation of two pipe diffuser configurations for a compact centrifugal compressor, PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2018, 第 5 作者
（20） 跨音速涡轮平面叶栅风洞收缩段设计方法研究, Wind Tunnel Contraction Design for Transonic Turbine Linear Cascade Test, 燃气轮机技术, 2017, 第 3 作者
（21） 离心压气机管式扩压器研究进展及评述, A review of studies on pipe diffuser of centrifugal compressor, 航空学报, 2017, 第 2 作者
（22） Design and Experimental Test of a 2.5-Stage Highly Loaded Axial Compressor, Proceedings of Shanghai 2017 Global Power and Propulsion Forum, 2017, 第 1 作者
（23） 级负荷系数为0.42的小流量轴流压气机设计与试验验证, Design and Measurements for a Small Flow Rate Axial Compressor with Stage Work Coefficient of 0.42, 航空发动机, 2016, 第 2 作者
（24） 跨声速压气机多圆柱孔式处理机匣设计与扩稳机理研究, Design and Investigation of Multiple Cylinder Holes Casing Treatment for Transonic Axial Compressor, 推进技术, 2015, 第 1 作者
（25） 一种涡轮叶尖间隙控制技术, A tip clearance control technology for turbine, 航空动力学报, 2014, 第 5 作者
（26） 喉部长度和扩张角对离心压气机管式扩压器影响研究, Effects of Diffuser Throat Length and Divergence Angle on Performance of Centrifugal Compressor with Pipe Diffuser, 推进技术, 2014, 第 4 作者
（27） Investigation on Multiple Cylindrical Holes Casing Treatment for Transonic Axial Compressor Stability Enhancement, JOURNAL OF THERMAL SCIENCE, 2014, 通讯作者
（28） 喉部长度和扩张角对离心压气机管式扩压器影响研究, 推进技术, 2014, 第 4 作者
（29） Parametric Studies of Pipe Diffuser on Performance of a Highly Loaded Centrifugal Compressor, JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2014, 第 4 作者

   

现指导学生

唐宇安  硕士研究生  082502-航空宇航推进理论与工程  

邓坤盈  硕士研究生  085800-能源动力