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

2025-06--中国科学院工程热物理研究所   正高级工程师
2019-05--2025-06   中国科学院工程热物理研究所   高级工程师
2015-07--2019-05   中国科学院工程热物理研究所   助理研究员
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
2010-07--2012-08   中国航发湖南动力机械研究所   设计员
2008-09--2010-06   东北大学   研究生，工学硕士
2004-09--2008-06   沈阳航空工业学院   本科，工学学士

研究生

工学博士

   

2025-06~现在, 中国科学院工程热物理研究所, 正高级工程师
2019-05~2025-06,中国科学院工程热物理研究所, 高级工程师
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

2023-06-01-今,国家科技部项目评审专家,
2023-04-06-今,北京市科技项目评审专家,

流体动力学测试技术

   

（1） Integrated optimization and thermodynamic characteristic analysis of adjustable splitter in a variable cycle compression system, APPLIED THERMAL ENGINEERING, 2025, 第 6 作者
（2） 涵道调节对新型变循环压缩系统匹配特性的影响研究, Research on the Influence of Bypass Adjustment on Matching Characteristics of a Novel Variable Cycle Compression System, 工程热物理学报, 2025, 第 4 作者
（3） The Matching Mechanism and Flow Mechanisms of Supersonic Through-Flow Variable-Pitch Tandem Cascade, JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2025, 第 6 作者
（4） 静子轮毂间隙对核心驱动风扇内部流动影响研究, Effects of clearance in stator hub on internal flow of core-driven fans, 推进技术, 2025, 第 2 作者
（5） Effect of double bypass conditions on the thermodynamic characteristics and internal flow mechanisms in a variable core cycle compression system, ENERGY, 2024, 第 6 作者
（6） Influence of diversified dihedral stator on the thermodynamic performance and flow loss characteristics of a variable core driven fan stage, ENERGY, 2024, 第 5 作者
（7） Effect of variable inlet guide vanes on thermodynamic characteristic and flow mechanism of a core compression system for variable cycle engine, PHYSICS OF FLUIDS, 2024, 第 6 作者
（8） Loss reduction in the compressor corner region via blade cooling, INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES, 2024, 第 3 作者
（9） 壁面换热条件下高负荷压气机叶片分离剪切层转捩机理研究, Numerical Investigations on the Transition Within Separated Shear Layers Over Highly Loaded Compressor Blades With Heat Transfer, 工程热物理学报, 2023, 第 2 作者
（10） 采用多层次优化方法的超紧凑GTF增压级气动设计, Aggressive GTF booster aerodynamic design with multi-level optimization method, 航空动力学报, 2023, 第 3 作者
（11） Robust aerodynamic optimization and design exploration of a wide-chord transonic fan under geometric and operational uncertainties, ENERGY, 2023, 第 6 作者
（12） Control of separated flow transition over a highly loaded compressor blade via dynamic surface deformation, INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES, 2023, 第 3 作者
（13） Effects of Bionic Leading Edge on the Aerodynamic Performance of a Compressor Cascade at a Low Reynolds Number, JOURNAL OF THERMAL SCIENCE, 2023, 第 4 作者
（14） The investigation of mechanisms on pipe diffuser leading edge vortex generation and development in centrifugal compressor, APPLIED THERMAL ENGINEERING, 2023, 第 2 作者
（15） Loss Reduction in the Compressor Corner Region via Blade Cooling, International Journal of Mechanical Sciences, 2023, 第 3 作者
（16） The investigation of mechanisms on pipe diffuser leading edge vortex generation and development in centrifugal compressor, Applied Thermal Engineering, 2022, 第 2 作者
（17） Control of separated flow transition over a highly loaded compressor blade via dynamic surface deformation, International Journal of Mechanical Sciences, 2022, 第 3 作者
（18） Research on aerodynamic optimization design method and flow mechanism of a high-subsonic compressor cascade, ENGINEERING APPLICATIONS OF COMPUTATIONAL FLUID MECHANICS, 2022, 第 6 作者  通讯作者
（19） Vortex dynamics and entropy generation in separated transitional flow over a compressor blade at various incidence angles, Vortex dynamics and entropy generation in separated transitional flow over a compressor blade at various incidence angles, CHINESE JOURNAL OF AERONAUTICS, 2022, 第 4 作者
（20） 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
（21） 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, 第 2 作者  通讯作者
（22） 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
（23） Numerical investigation of distributed roughness effects on separated flow transition over a highly loaded compressor blade, PHYSICS OF FLUIDS, 2021, 第 3 作者
（24） 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
（25） 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
（26） 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
（27） Numerical investigations of the separated transitional flow over compressor blades with different loading distributions, AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 第 3 作者
（28） 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
（29） 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
（30） 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
（31） Numerical and experimental investigation of flow mechanism and application of tandem-impeller for centrifugal compressor, AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 第 5 作者
（32） 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
（33） 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, 第 2 作者  通讯作者
（34） 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
（35） DESIGN AND TEST OF A NOVEL HIGHLY-LOADED COMPRESSOR, PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2019, VOL 2A, 2019, 第 1 作者  通讯作者
（36） 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
（37） 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
（38） 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
（39） 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
（40） 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
（41） 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
（42） 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
（43） Numerical Investigation of a Cantilevered Compressor Stator at Varying Clearance Sizes, ASME, 2015, 第 1 作者
（44） 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
（45） Effects of low Reynolds number on flow stability of a transonic compressor, PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2015, 第 5 作者
（46） 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
（47） 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
（48） Investigation on Multiple Cylindrical Holes Casing Treatment for Transonic Axial Compressor Stability Enhancement, JOURNAL OF THERMAL SCIENCE, 2014, 第 1 作者  通讯作者
（49） 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
（50） 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

已指导学生

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  

现指导学生

赵明旻  硕士研究生  085800-能源动力  

陆易  硕士研究生  082502-航空宇航推进理论与工程