基本信息
张宏武 男 博导 中国科学院工程热物理研究所
电子邮件: zhw@mail.etp.ac.cn
通信地址: 北四环西路11号
邮政编码:
电子邮件: zhw@mail.etp.ac.cn
通信地址: 北四环西路11号
邮政编码:
招生信息
招生专业
080703-动力机械及工程
招生方向
叶轮机械工程热物理航空宇航推进理论与工程
教育背景
1996-09--2000-06 清华大学 博士1992-09--1995-06 华东工业大学 硕士1988-09--1992-07 上海机械学院 学士
工作经历
工作简历
1996-09~2000-06,清华大学, 博士1992-09~1995-06,华东工业大学, 硕士1988-09~1992-07,上海机械学院, 学士
专利与奖励
专利成果
( 1 ) 压气机试验设备, 2022, 第 5 作者, 专利号: 202211019580.X( 2 ) 动态传感器与机匣处理一体化结构、压气机机匣及压气机, 2022, 第 3 作者, 专利号: CN215980058U( 3 ) 压气机试验件结构, 2022, 第 6 作者, 专利号: CN111312058B( 4 ) 一种轴向缝式处理机匣, 2021, 第 4 作者, 专利号: CN110886724B( 5 ) 轴流压气机叶片及应用其的轴流压气机, 2021, 第 3 作者, 专利号: CN113048098A( 6 ) 一种微型动态传感器与机匣处理一体化结构, 2021, 第 3 作者, 专利号: CN112963370A( 7 ) 一种升压变压器、升压方法及升压电路, 2021, 第 2 作者, 专利号: CN112953248A( 8 ) 一种压气机进口导叶角度实时调节装置, 2021, 第 7 作者, 专利号: CN212774919U( 9 ) 一种压气机试验瞬态畸变调节装置, 2021, 第 6 作者, 专利号: CN212744290U( 10 ) 可调叶片密封结构, 2021, 第 7 作者, 专利号: CN112343854A( 11 ) 一种压气机叶型设计方法及压气机叶型, 2021, 第 7 作者, 专利号: CN112347579A( 12 ) 测试轴流压气机瞬态总压畸变的畸变发生装置, 2020, 第 5 作者, 专利号: CN212130862U( 13 ) 压气机前窄后宽式缝式处理机匣装置, 2020, 第 5 作者, 专利号: CN212130883U( 14 ) 压气机用畸变发生器承力框架, 2020, 第 5 作者, 专利号: CN210513705U( 15 ) 一种自适应主动控制的叶片及其制作方法, 2020, 第 5 作者, 专利号: CN111102249A( 16 ) 采用自适应康达喷气的叶片及制作方法, 2020, 第 4 作者, 专利号: CN111102012A( 17 ) 基于自适应网格的二维叶型优化设计方法及装置, 2020, 第 6 作者, 专利号: CN110851929A( 18 ) 压气机用畸变发生器承力框架, 2019, 第 5 作者, 专利号: CN110595788A( 19 ) 采用自适应康达喷气的叶片, 2019, 第 4 作者, 专利号: CN209444376U( 20 ) 一种等离子体压力传感器及压力传感系统, 2019, 第 4 作者, 专利号: CN110243536A( 21 ) 一种进气道结构及其制作方法, 2019, 第 5 作者, 专利号: CN110206666A( 22 ) 压气机稳定性预测方法, 2019, 第 4 作者, 专利号: CN110162858A( 23 ) 一种自适应主动控制的叶片, 2019, 第 5 作者, 专利号: CN209228724U( 24 ) 一种进气道结构及其制作方法, 2019, 第 5 作者, 专利号: CN110043368A( 25 ) 一种轴流压气机叶片及轴流压气机, 2019, 第 4 作者, 专利号: CN209129924U( 26 ) 一种轴流压气机叶片及轴流压气机, 2019, 第 4 作者, 专利号: CN209129924U( 27 ) 静叶间自循环抽吸喷气的多级轴流压气机, 2018, 第 5 作者, 专利号: CN108661953A( 28 ) 采用康达喷气的轴流压气机叶片及应用其的轴流压气机, 2018, 第 5 作者, 专利号: CN108661947A( 29 ) 等离子体压力传感器及等离子体压力传感系统, 2018, 第 5 作者, 专利号: CN107727310A( 30 ) 等离子体压力传感器及系统, 2018, 第 5 作者, 专利号: CN107727311A( 31 ) 一种动态五孔探针, 2017, 第 6 作者, 专利号: CN206725183U( 32 ) 基于直流辉光放电等离子体原理的高频响压力传感器, 2017, 第 4 作者, 专利号: CN107389255A( 33 ) 在线标定和补偿的动态测量系统及方法, 2017, 第 5 作者, 专利号: CN107289985A( 34 ) 一种动态五孔探针, 2017, 第 6 作者, 专利号: CN107101798A( 35 ) 压气机机匣及应用其的轴流压气机, 2017, 第 4 作者, 专利号: CN106870461A( 36 ) 一种压气机、燃气轮机及压气机扩稳增效方法, 2017, 第 5 作者, 专利号: CN106870465A( 37 ) 一种压气机气动稳定性诊断和控制的装置及方法, 2017, 第 4 作者, 专利号: CN106640722A( 38 ) 微型航空发动机轴承燃油换热冷却装置, 2015, 第 4 作者, 专利号: CN104265460A( 39 ) 微型航空发动机轴承多点喷射油雾润滑冷却装置, 2014, 第 4 作者, 专利号: CN104196632A( 40 ) 一种燃气轮机贫预混燃烧室, 2013, 第 2 作者, 专利号: CN202813443U( 41 ) 一种燃气轮机贫预混燃烧室, 2013, 第 2 作者, 专利号: CN102878580A( 42 ) 非热力学平衡等离子体点火与助燃装置, 2010, 第 1 作者, 专利号: CN101761940A( 43 ) 叶片式流体机械的导叶、静叶、转速可调三因素匹配方法, 2010, 第 3 作者, 专利号: CN101311554B( 44 ) 中/小型燃气轮机在线故障诊断、预测、反馈控制方法及装置, 2010, 第 1 作者, 专利号: CN101694182A( 45 ) 叶片式流体机械节能增效的三因素匹配方法, 2008, 第 3 作者, 专利号: CN101311554A
出版信息
发表论文
(1) Optimized casing treatment to improve stall margin under circumferential pressure distortion in a high-speed axial flow fan, JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2024, 第 7 作者(2) Design Optimization of 1.5-Stage Transonic Compressor Based on BPNN Surrogate Model and NSGA-II, MACHINES, 2023, 第 6 作者(3) Optimization Design of Aspect Ratio and Solidity of a Heavy-Duty Gas Turbine Transonic Compressor Rotor, MACHINES, 2023, 第 5 作者(4) 航空发动机部件和整机通流数值模拟研究, Numerical Study on Throughflow Simulation of Components and Full Engine of Aero-Engine, 工程热物理学报, 2023, 第 4 作者(5) Design Optimization and Analysis of Exit Rotor with Diffuser Passage based on Neural Network Surrogate Model and Entropy Generation Method, Design Optimization and Analysis of Exit Rotor with Diffuser Passage based on Neural Network Surrogate Model and Entropy Generation Method, JOURNAL OF THERMAL SCIENCE, 2023, 第 5 作者(6) Adaptive feedback control of stability in an axial compressor with circumferential inlet distortion, Adaptive feedback control of stability in an axial compressor with circumferential inlet distortion, CHINESE JOURNAL OF AERONAUTICS, 2023, 第 5 作者(7) Design Optimization and Analysis of Exit Rotor with Diffuser Passage based on Neural Network Surrogate Model and Entropy Generation Method, Journal of Thermal Science, 2023, 第 5 作者(8) Optimization Design of Aspect Ratio and Solidity of Heavy-Duty Gas Turbine Transonic Compressor Rotor, Machines, 2023, 第 5 作者(9) Influence of Hub Contouring on the Performance of a Transonic Axial Compressor Stage with Low Hub-Tip Ratio, Journal of Thermal Science, 2022, 第 4 作者(10) 径向畸变条件下轴向缝机匣处理扩稳实验研究, Axial Slot Casing Treatment for Stall Margin Improvement in an Axial Flow Compressor With Radial Distortion, 工程热物理学报, 2022, 第 5 作者(11) ADAPTIVE FEEDBACK CONTROL OF STABILITY IN AN AXIAL FLOW COMPRESSOR WITH CIRCUMFERENTIAL INLET DISTORTION, The First International Conference on Mechanical System Dynamics, 2022, 第 4 作者(12) 高负荷压气机叶栅流动分离的主动控制方法综述, Active Flow Control Concepts of Secondary Flow on a Highly Loaded Compressor Cascade, 工程热物理学报, 2022, 第 5 作者(13) Design Optimization of Exit stage with Diffuser Passage based on NSGA-��� and Kriging Surrogate Model, The First International Conference on Mechanical System Dynamics, 2022, 第 4 作者(14) Stall Warning Strategy Based on Fast Wavelet Analysis in a Multistage Axial Flow Compressor, JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2022, 第 4 作者(15) 旋转畸变对压气机稳定性影响实验研究, 中国工程热物理学会 热机气动热力学 学术会议论文, 2022, 第 4 作者(16) 多级轴流压气机出口级转子扩张通道优化设计, Design optimization of exit stage rotor with diffuser passage in multi-stage axial compressor, 航空动力学报, 2022, 第 5 作者(17) Aerodynamic Performance Improvement of a Highly Loaded Compressor Airfoil with Coanda Jet Flap, Aerodynamic Performance Improvement of a Highly Loaded Compressor Airfoil with Coanda Jet Flap, JOURNAL OF THERMAL SCIENCE, 2022, 第 5 作者(18) Influence of Hub Contouring on the Performance of a Transonic Axial Compressor Stage with Low Hub-Tip Ratio, Influence of Hub Contouring on the Performance of a Transonic Axial Compressor Stage with Low Hub-Tip Ratio, JOURNAL OF THERMAL SCIENCE, 2022, 第 4 作者(19) 多级轴流压气机出口级转子扩张通道优化设计, 航空动力学报, 2021, 第 1 作者(20) Implementation of stability-enhancement with tip air injection in a multi-stage axial flow compressor, AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 第 4 作者(21) Physical Mechanisms Investigation of Sharkskin-Inspired Compressor Cascade Based on Large Eddy Simulations, JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2021, 第 4 作者(22) Reliability analysis for stall warning methods in an axial flow compressor, AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 第 4 作者(23) A study of fan-distortion interaction within the fan rotor, PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2021, 第 5 作者(24) Implement of Stability-Enhancement with Tip Air Injection in a Multi-Stage Axial Flow Compressor, Aerospace Science and Technology, 2021, 第 1 作者(25) Stall Warning Strategy Based on Fast Wavelet Analysis in a Multi-Stage Axial Flow Compressor., Journal of Engineering for Gas Turbine and Power, 2021, 第 1 作者(26) Tip Air Injection to Extend the Stall Margin on an Axial Compressor with Circumferential Distortion, JOURNAL OF THERMAL SCIENCE, 2021, 第 1 作者(27) Dual stability enhancement mechanisms of axial-slot casing treatment in a high-speed mixed-flow compressor with various tip clearances, Dual stability enhancement mechanisms of axial-slot casing treatment in a high-speed mixed-flow compressor with various tip clearances, CHINESE JOURNAL OF AERONAUTICS, 2021, 第 5 作者(28) Tip air injection to extend stall margin of multi-stage axial flow compressor with inlet radial distortion, AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 第 5 作者(29) Automatic stability control using tip air injection in a multi-stage axial flow compressor, AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 第 4 作者(30) Design optimization of axial slot casing treatment in a highly-loaded mixed-flow compressor, AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 第 5 作者(31) 周向畸变下轴流压气机的失速预警方法研究及应用, Stall Warning Method Investigation and Application in an Axial-Flow Compressor with Circumferential Distortion, 推进技术, 2020, 第 4 作者(32) Effect of inlet radial distortion on aerodynamic stability in a multi-stage axial flow compressor, AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 第 4 作者(33) Dual Stability Enhancement Mechanisms of Axial-Slot Casing Treatment in a HighSpeed Mixed-Flow Compressor with Various Tip Clearances, Chinese Journal of Aeronautics, 2020, 第 1 作者(34) 基于B样条的斜流压气机机匣处理优化设计, Design and Optimization of Casing Treatment Based on B-spline Curves in a Mixed-Flow Compressor, 工程热物理学报, 2020, 第 5 作者(35) 周向畸变下周轴流压气机的失速预警方法研究及应用, 推进技术, 2020, 第 1 作者(36) 空气湿度对舰用燃气轮机两级对置式离心压气机性能的影响, Humidity effects on the performance of an opposed-setting-two-stage centrifugal compressor for marine gas turbine, 舰船科学技术, 2020, 第 4 作者(37) Performance enhancement of industrial high loaded gas compressor using Coanda jet flap, ENERGY, 2019, 第 6 作者(38) "Irreversible Loss Analysis of Tip Leakage Flow in a Gas Turbine Compressor, ENTROPY, 2019, 第 1 作者(39) Stability enhancement using a new hybrid casing treatment in an axial flow compressor, AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 第 5 作者(40) Circumferentially propagating characteristic dominated by unsteady tip leakage flow in axial flow compressors, AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 第 4 作者(41) Application of Fast Wavelet Analysis on Early Stall Warning in Axial Compressors, Application of Fast Wavelet Analysis on Early Stall Warning in Axial Compressors, JOURNAL OF THERMAL SCIENCE, 2019, 第 5 作者(42) Review of tip air injection to improve stall margin in axial compressors, PROGRESS IN AEROSPACE SCIENCES, 2019, 第 4 作者(43) Special column for the memory of Professor CHEN Naixing, Special column for the memory of Professor CHEN Naixing, JOURNAL OF THERMAL SCIENCE, 2019, 第 2 作者(44) 斜流压气机轴向缝机匣处理设计及扩稳机理研究, Design and Stability Enhancement Mechanism of Axial-Slot Casing Treatment on a Mixed-Flow Compressor, 工程热物理学报, 2019, 第 4 作者(45) IMPROVING AERODYNAMIC PERFORMANCE OF A HIGHLY LOADED COMPRESSOR BASED ON COANDA JET FLAP, PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2019, VOL 2A, 2019, 第 6 作者(46) Entropy Generation Analysis in a Mixed-Flow Compressor with Casing Treatment, Entropy Generation Analysis in a Mixed-Flow Compressor with Casing Treatment, JOURNAL OF THERMAL SCIENCE, 2019, 第 5 作者(47) 两级对置式离心压气机湿压缩研究, Wet Compression Effects on an Opposed-Setting-Two-Stage Centrifugal Compressor, 推进技术, 2019, 第 3 作者(48) Quantification and Analysis of the Irreversible Flow Loss in a Linear Compressor Cascade, ENTROPY, 2018, 第 4 作者(49) 通过熵产率构建的两类损失模型计算精度比较, Accuracy Comparison of Two Entropy Generation Rate Models Based on the RANS/LES Method, 工程热物理学报, 2018, 第 4 作者(50) Influence of Rain Ingestion on the Endwall Treatment in an Axial Flow Compressor, JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2018, 第 5 作者(51) 可以恢复Navier-Stokes方程的3阶格子Boltzmann作用力模型, A third order lattice Boltzmann force model capable of recoving the Naveir-Stokes equations, 航空动力学报, 2017, 第 2 作者(52) 熔盐-气体换热器传热性能的实验研究, EXPERIMENTAL INVESTIGATION FOR HEAT PERFORMANCE OF MOLTEN SALT-GAS HEAT EXCHANGER, 太阳能学报, 2017, 第 4 作者(53) A comparative study of boundary conditions for lattice Boltzmann simulations of high Reynolds number flows, COMPUTERS AND FLUIDS, 2017, 第 3 作者(54) 熔盐换热器流动传热性能实验系统, An Experimental System for Performances of Molten Salt Heat Exchangers, 中国电机工程学报, 2017, 第 3 作者(55) 来流边界层对压气机平面叶栅角区流动的影响, Effects of Inlet Boundary Layer on Corner Flow in a Linear Compressor Cascade, 推进技术, 2017, 第 3 作者(56) Experimental study for shell-and-tube molten salt heat exchangers, APPLIED THERMAL ENGINEERING, 2017, 第 3 作者(57) A comparative study of boundary conditions for lattice Boltzmann simulations of high Reynolds number flows, COMPUTERS & FLUIDS, 2017, 第 3 作者(58) 压气机静叶栅层流分离泡转捩与角区分离数值模拟与实验, Numerical simulation and experiment of laminar separation bubble transition and corner separation of compressor stator cascade, 航空动力学报, 2017, 第 3 作者(59) 基于二维紧凑型四阶格子模型的激波管流动模拟, Simulating shock-tube flow with a two-dimensional compact fourth order lattice model, 航空动力学报, 2017, 第 3 作者(60) 压气机静叶珊层流分离泡转捩与角区分离数值模拟与实验, 航空动力学报, 2017, 第 1 作者(61) Second-Law Analysis of Irreversible Losses in Gas Turbines, ENTROPY, 2017, 第 4 作者(62) 粗糙度对压气机叶栅损失特性影响的实验研究, Experimental Study for Effects of Surface Roughness on Compressor Cascade Loss Characteristics, 推进技术, 2016, 第 4 作者(63) 叶栅倒角对压气机角区流动影响的数值模拟和实验研究, Numerical and Experimental Study of the Influence of Fillets on Compressors Corner Flow, 工程热物理学报, 2016, 第 4 作者(64) 翅片管式溶盐-气体换热器传热性能的实验研究, Experimental Study for a Finned Tube Molten Salt to Gas Heat Exchanger, 工程热物理学报, 2016, 第 3 作者(65) Performance of a gas cooled molten salt heat exchanger, APPLIED THERMAL ENGINEERING, 2016, 第 3 作者(66) 间隙变化对压气机静叶叶栅气动性能的影响, Influence of clearance variation on aerodynamic performance of a compressor stator cascade, 航空学报, 2016, 第 3 作者(67) 间隙和转速对轴流压气机非定常叶顶泄漏流周向传播特性影响的实验研究, Experimental Study of Effects of Tip Clearance and Shaft Speed on Circumferential Propagation Characteristics of Unsteady Tip Leakage Flow, 工程热物理学报, 2016, 第 4 作者(68) Decoupled scheme based on the Hermite expansion to construct lattice Boltzmann models for the compressible Navier-Stokes equations with arbitrary specific heat ratio, PHYSICAL REVIEW E, 2016, 第 2 作者 通讯作者(69) 压气机二维动叶栅流场非定常波动的大涡模拟, 航空动力学报, 2015, 第 1 作者(70) 间隙和转速对轴流压气机非定常叶顶泄漏流周向传播特性影响的实验研究, 2015年中国工程热物理学会气动学学术年会, 2015, 第 4 作者(71) 叶栅倒角对压气机角区流动影响的数值模拟和实验研究, 2015年中国工程热物理学会气动学学术年会, 2015, 第 4 作者(72) Tip Leakage Flow Unsteadiness and its Propagation Features in Axial Compressor: Effect of Inlet Hub Distortion, International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows, 2015, 第 1 作者(73) 压气机二维动叶栅非定常流场的大涡模拟, Large eddy simulation of unsteady flow field in a two-dimensional moving compressor cascade, 航空动力学报, 2015, 第 3 作者(74) 不同端壁间隙下压气机平面叶栅角区流动的数值模拟和实验研究, Numerical and Experimental Investigation on Corner Flow Structure in a Planar Compressor Cascade With Different Clearances, 工程热物理学报, 2015, 第 4 作者(75) 不同端壁间隙下压气机平面叶栅角区流动的数值模拟研究, 2014年工程热物理学会, 2014, 第 1 作者(76) Numerical Investigation on Interaction between Hub Clearance Flow and Corner Separation in a Planar Compressor Cascade, Asian Congress on Gas Turbines, 2014, 第 1 作者(77) 高温FLiNaK熔盐光滑圆管内湍流流动传热特性的数值模拟, 2014年中国工程热物理学会, 2014, 第 2 作者(78) 基于目标压力分布的压气机叶型黏性反问题设计方法, Viscous Inverse Design Method for Compressor Profile Based on Target Pressure Distribution, 汽轮机技术, 2014, 第 3 作者(79) 表面粗糙度对压气机叶栅性能影响的数值研究, 2014年工程热物理学会, 2014, 第 4 作者(80) 带无叶扩压器离心压气机的稳定性分析, Stability Analysis of Centrifugal Compressor with Vaneless Diffuser, 动力工程学报, 2013, 第 3 作者(81) Evolution of Pressure Signature Dominated by Unsteady Tip Leakage Flow, ASME, 2013, 第 4 作者(82) 对旋式轴流风机变转速匹配性能研究, Numerical study on matching performance of contra-rotating axial flow fan under variable speed, 机械设计与制造, 2012, (83) 基于NURBS曲线的轴流透平叶片气动数值优化, Numerical aerodynamic optimization of axial turbomachinery blades based on NURBS, 航空动力学报, 2012, 第 3 作者(84) A Study of the Unsteady Tip Flow Field of a Transonic Compressor, A Study of the Unsteady Tip Flow Field of a Transonic Compressor, JOURNAL OF THERMAL SCIENCE, 2011, 第 3 作者(85) 间隙大小与流量对轴流压气机平面叶栅叶顶泄漏流影响的实验研究, 中国工程热物理学会(热机气动热力学), 2011, 第 2 作者(86) 某F级燃气轮机压气机跨音级特性计算, Performance Prediction of the Transonic Compressor Stage of a Class F Gas Turbine, 燃气轮机技术, 2011, 第 2 作者(87) A Study of the Unsteady Tip Flow Field of a Transonic Compressor, A Study of the Unsteady Tip Flow Field of a Transonic Compressor, 热科学学报:英文版, 2011, 第 3 作者(88) 不同叶轮形式下离心泵噪声特性对比研究, Comparison of noise characteristics in centrifugal pumps with different types of impellers, 声学学报, 2010, 第 6 作者(89) 跨声速轴流压气机间隙泄漏流触发旋转失速, Tip leakage flow trigger rotating stall in a transonic axial-flow compressor, 推进技术, 2010, 第 4 作者(90) 某F级燃气轮机压气机跨音级校核计算, 中国工程热物理学会(热机气动热力学), 2010, 第 2 作者(91) Numerical Investigation on the Self-Induced Unsteadiness in Tip Leakage Flow for a Transonic Fan Rotor, JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2010, 第 3 作者(92) 低速单转子轴流压气机突尖型失速特征, CHARACTERISTICS OF SPIKE TYPE ROTATING STALL IN A LOW SPEED ISOLATED AXIAL COMPRESSOR ROTOR, 工程热物理学报, 2010, 第 3 作者(93) Denton程序对汽轮机低压缸流场模拟的校核与分析, Numerical Validation and Analysis of Denton Program for the Low-pressure Cylinder of Steam Turbine, 汽轮机技术, 2010, 第 2 作者(94) 基于NURBS曲线和遗传算法的轴流透平叶片气动优化设计, 中国工程热物理学会(热机气动热力学), 2010, 第 3 作者(95) Investigation for the Effects of Circumferential Grooves on the Unsteadiness of Tip Clearance Flow to Enhance Compressor Flow Instability, ASME:Turbomachinery: Axial Flow Fan & Compressor Aerodynamics, 2010, (96) 不同叶轮形式下离心泵噪声特性对比研究, 中国工程热物理会(气动), 2009, 第 3 作者(97) 1000MW超超临界汽轮机中压缸进汽蜗壳的数值模拟研究, Numerical Simulation on the Steam Admission Volute in the Intermediate Pressure Cylinder of 1 000MW Ultra Supercritical Steam Turbine, 汽轮机技术, 2009, 第 4 作者(98) 三级轴流压气机变工况条件下导叶/静叶和转速联动的调节规律, Investigation on the aerodynamic adjustment between inlet guide-vane,stator,and operating speed of three-stage axial compressor, 航空动力学报, 2009, 第 2 作者(99) 吸附式叶栅代替串联叶栅气动可行性探索, EXPLORING THE AERODYNAMIC FEASIBILITY OF SUBSTITUTING ASPIRATED CASCADE FOR TANDEM CASCADE, 工程热物理学报, 2009, 第 4 作者(100) 周向槽调控轴流压气机非定常间隙泄漏流机理初探, 中国工程热物理会(气动), 2009, 第 3 作者(101) Denton程序对某汽轮机低压缸流场模拟及对比分析, 中国工程热物理会(气动), 2009, 第 2 作者(102) Circumferential propagation of tip leakage flow unsteadiness for a low-speed axial compressor, JOURNAL OF THERMAL SCIENCE,, 2009, 第 4 作者(103) 某跨音速轴流压气机转子叶顶泄漏流的非定常特征, NUMERICAL SIMULATION ON UNSTEADY TIP LEAKGAE FLOW IN A TRANSONIC AXIAL FAN ROTOR, 工程热物理学报, 2009, 第 3 作者(104) 跨音速轴流压气机叶顶间隙泄漏流对微喷气的非定常响应机制和扩稳效果研究, UNSTEADY RESPONSE OF TIP LEAKAGE FLOW TO DISCRETE MICRO TIP INJECTION IN A TRANSONIC AXIAL COMPRESSOR AND ITS EFFECT ON STABILITY ENHANCEMENT, 工程热物理学报, 2009, 第 2 作者(105) 跨音速涡轮叶栅叶型损失预测, Profile Losses Prediction of Transonic Turbine Cascades, 汽轮机技术, 2009, 第 3 作者(106) 亚音速轴流压气机转子非轴对称轮毂端壁的数值研究, NUMERICAL INVESTIGATION ON A SUBSONIC AXIAL-FLOW COMPRESSOR ROTOR WITH THE IMPLEMENTATION OF NON-AXIASYMMETRIC HUB END WALL, 工程热物理学报, 2009, 第 3 作者(107) Circumferential Propagation of Tip Leakage Flow Unsteadiness for a Low-Speed Axial Compressor, Circumferential Propagation of Tip Leakage Flow Unsteadiness for a Low-Speed Axial Compressor, JOURNAL OF THERMAL SCIENCE, 2009, 第 4 作者(108) 1000MW超超临界汽轮机中压缸第一级斜置静叶的数值模拟研究, Numerical Simulation on the First Stage Oblique Stator in the Intermediate Pressure Cylinder of 1 000 MW Uhra Supercritical Steam Turbine, 汽轮机技术, 2009, 第 4 作者(109) 低速单转子轴流压气机突尖型失速特征, 中国工程热物理会(气动), 2009, 第 3 作者(110) 吸附式叶栅代替串联叶栅可行性探索研究, 中国工程热物理会(热力学), 2008, 第 4 作者(111) 跨音速轴流风扇转子叶顶泄漏流的数值研究, NUMERICAL SIMULATION ON UNSTEADY TIP LEAKAGE FLOW IN A TRANSONIC AXIAL FAN ROTOR, 工程热物理学报, 2008, 第 3 作者(112) 轴流压气机转子非轴对称轮毂端壁的数值研究, 中国工程热物理会(热力学), 2008, 第 3 作者(113) 跨音速轴流压气机转子叶顶泄漏流的非定常特征第二部分:某跨音速轴流压气机, 中国工程热物理会(热力学), 2008, 第 3 作者(114) Numerical Simulation on the Effect of Tip Clearance Size on Unsteadiness in Tip Clearance Flow, Numerical Simulation on the Effect of Tip Clearance Size on Unsteadiness in Tip Clearance Flow, 热科学学报:英文版, 2008, 第 3 作者(115) 某汽轮机中压缸流场的快速分析, The Quick Numerical Simulation of A Multistage Turbine, 汽轮机技术, 2008, 第 3 作者(116) Numerical Investigation on the Originating Mechanism of Unsteadiness in Tip Leakage Flow for a Transonic Fan Rotor, ASME:Turbomachinery: Axial Flow Fan and Compressor Aerodynamics, 2008, (117) 前掠提高跨音速压气机转子失速裕度的机理研究, 中国工程热物理会(热力学), 2008, 第 3 作者(118) 跨音速轴流压气机叶顶间隙泄漏流对微喷气的非定常响应机制和扩稳效果研究, 中国工程热物理会(热力学), 2008, 第 2 作者(119) 基于Denton程序的某汽轮机中压缸流场的多级联算, Numerical Simulation of a Multistage Turbine Based on Denton, 热力透平, 2008, 第 4 作者(120) Numerical Simulation on the Effect of Tip Clearance Size on Unsteadiness in Tip Clearance Flow, JOURNAL OF THERMAL SCIENCE, 2008, 第 3 作者(121) 跨音速轴流压气机转子叶顶泄漏流的非定常特征第一部分 NASA Rotor37跨音速轴流压气机, 中国工程热物理会(热力学), 2008, 第 2 作者(122) 旋转进口畸变与轴流压气机旋转失速相关联的模型与实验探索, EXPERIMENTAL AND MODEL INVESTIGATION OF THE CORRELATION BETWEEN ROTATING INLET DISTORTION AND ROTATING STALL OF AN AXIAL COMPERSSOR, 工程热物理学报, 2007, 第 3 作者(123) Numerical Simulation of Rotating Stall in a Centrifugal Compressor with Vaned Diffuser, Numerical Simulation of Rotating Stall in a Centrifugal Compressor with Vaned Diffuser, JOURNAL OF THERMAL SCIENCE, 2007, 第 4 作者(124) Numerical study on the response of tip leakage flow unsteadiness to micro tip injection in a low-speed isolated compressor rotor, ASME Paper No.GT2007-27729, 2007, 第 1 作者(125) 吸附式跨声速压气机叶栅流场数值模拟, Numerical investigation of boundary layer suction in an axial transonic compressor cascade, 航空动力学报, 2007, 第 4 作者(126) Blade Parameterization and Aerodynamic Design Optimization for a 3D Transonic Compressor Rotor, Blade Parameterization and Aerodynamic Design Optimization for a 3D Transonic Compressor Rotor, JOURNALOFTHERMALSCIENCE, 2007, 第 2 作者(127) 喷气对低速轴流压气机转子叶顶区域流动的影响, EFFECTS OF MICRO AIR INJECTION ON ROTOR TIP FLOW IN A LOW-SPEED ISOLATED AXIAL COMPRESSOR ROTOR, 工程热物理学报, 2007, 第 2 作者(128) 汽轮机排气缸流场的数值模拟研究, 3D Flow-Field Study of the Steam Turbine Exhaust Hood by Numerical Simulation, 热力透平, 2007, 第 3 作者(129) Numerical Simulation of Rotating Stall in a Centrifugal Compressor with Vaned Diffuser, Numerical Simulation of Rotating Stall in a Centrifugal Compressor with Vaned Diffuser, 热科学学报:英文版, 2007, 第 4 作者(130) Unsteady tip clearance flow pattern in an isolated axial compressor rotor with micro tip injection, JOURNAL OF THERMAL SCIENCE, 2007, 第 2 作者(131) 压气机非定常叶顶间隙流的数值模拟研究, 工程热物理学报, 2006, 第 2 作者(132) The Response of a Low Speed Compressor on Rotating Inlet Distortion, JOURNAL OF THERMAL SCIENCE, 2006, 第 4 作者(133) 风扇/增压级非设计工况特性分析, 工程热物理学报, 2006, 第 2 作者(134) A Study on the Mechanism of Tip Leakage Flow Unsteadiness in an Isolated Compressor Rotor, ASME:TURBOMACHINERY: AXIAL FLOW FAN AND COMPRESSOR AERODYNAMICS, 2006, (135) 低速离心压气机的全工况数值模拟和校核, THE NUMERICAL SIMULATION AND VERIFICATION OF LOW-SPEED CENTRIFUGAL COMPRESSOR IN WHOLE FLOW-RATE RANGE, 工程热物理学报, 2005, 第 3 作者(136) Study on Aerodynamic Design Optimization of Turbomachinery Blades, Study on Aerodynamic Design Optimization of Turbomachinery Blades, JOURNAL OF THERMAL SCIENCE, 2005, 第 2 作者(137) 叶型中弧线的最大弯度位置对跨音速压气机叶片性能影响的研究, 工程热物理学报, 2005, 第 2 作者(138) 低速离心压气机的全工况数值模拟和校核, THE NUMERICAL SIMULATION AND VERIFICATION OF LOW-SPEED CENTRIFUGAL COMPRESSOR IN WHOLE FLOW-RATE RANGE, 工程热物理学报, 2005, 第 3 作者(139) 空冷汽轮机低压缸马刀叶片性能三维数值分析, 3D NUMERICAL SIMULATION OF BOWED BLADING IN LOW PRESSURE STEAM TURBINE AT DIFFERENT WORKING CONDITIONS, 工程热物理学报, 2005, 第 3 作者(140) 低速轴流压气机中前后静叶对动叶顶部区域流动的影响, Effects of Upstream and Downstream Stators on Rotor Tip Flow in a Low-speed Axial Compressor, 航空学报, 2005, 第 2 作者(141) 低速轴流压气机单转子旋转失速三维数值模拟和实验比较, COMPARISON OF NUMERICAL SIMULATION AND EXPERIMENT OF ROTATING STALL IN A LOW-SPEED AXIAL ROTOR COMPRESSOR, 工程热物理学报, 2005, 第 2 作者(142) 低速轴流压气机单转子旋转失速三维数值模拟和实验比较, COMPARISON OF NUMERICAL SIMULATION AND EXPERIMENT OF ROTATING STALL IN A LOW-SPEED AXIAL ROTOR COMPRESSOR, 工程热物理学报, 2005, 第 2 作者(143) 低速轴流压气机中工况变化对动叶顶部泄漏流波动频率的影响, EFFECTS OF OPERATING CONDITION ON THE FREQUENCY CHARACTERISTIC OF ROTOR TIP LEAKAGE FLOW IN AN LOW-SPEED AXIAL COMPRESSOR, 工程热物理学报, 2005, 第 2 作者(144) Unsteady Tip Clearance Flow in an Isolated Axial Compressor Rotor, Unsteady Tip Clearance Flow in an Isolated Axial Compressor Rotor, 热科学学报:英文版, 2005, 第 1 作者(145) 跨音速单转子压气机气动设计的优化, 工程热物理学报, 2005, 第 1 作者(146) Unsteady Tip Clearance Flow in an Isolated Axial Compressor Rotor, JOURNAL OF THERMAL SCIENCE, 2005, 第 1 作者 通讯作者(147) 航空发动机内外涵道三维粘性流场的数值模拟, 3-D VISCOUS NUMERICAL SIMULATION OF FAN-BYPASS-COMPRESSOR, 工程热物理学报, 2005, 第 2 作者(148) 叶顶间隙大小和壁面相对运动对低速轴流压气机孤立转子性能的影响, 工程热物理学报, 2004, 第 2 作者(149) Geometry Effects on Aerodynamics Performance of a Low Aspect Ratio Turbine Nozzle, JOURNAL OF THERMAL SCIENCE, 2004, 第 2 作者(150) A Study of 3D Aerodynamic Design for a Transonic Compressor Blading Optimized by the Locations of Aerofoil Maximum Thickness and Maximum Camber, JOURNAL OF THERMAL SCIENCE, 2003, 第 2 作者(151) 多级轴流压气机三维气动设计的一种快速方法, 工程热物理学报, 2003, 第 2 作者(152) 甲烷预混燃烧火焰的详细数值模拟, 工程热物理学报, 2002, 第 3 作者(153) 单级跨音压气机整圈三维动静叶干涉的数值模拟, Three-Dimensional Numerical Simulation of Whole-Ring Rotor/Stator Interaction in a Single-Stage Compressor, 航空动力学报, 2002, 第 3 作者(154) 叶轮机械内部复杂流动和数值模拟和三级低速轴流压气机设计, 2002, 第 1 作者(155) 跨音透平级动叶顶部间隙流动的数值模拟, 工程热物理学报, 2002, 第 1 作者(156) 透平级非设计工况气动性能的数值模拟, 工程热物理学报, 2001, 第 1 作者(157) 应用高分辨率迎风格式精确分析透平叶栅三维湍流流场, 工程热物理学报, 1999, 第 1 作者(158) Full-engine simulation of micro gas turbine based on time-marching throughflow method, APPLIED THERMAL ENGINEERING, 第 4 作者