马宏伟｜北京航空航天大学｜学者主页

2026

大尺寸多功能涡轮试验装置及测试系统

马宏伟，肖安琪，郭君德，范聪聪

《推进技术》

2026

Research on error analysis and compensation method of combined water-cooled rake for enhanced temperature measurement accuracy

Ruolin Gao, Hongwei Ma, Yue Shi, Qingdian Zhang

Measurement

DOI

2025

低速轴流压气机叶尖泄漏涡破碎研究

庞健，贺象，马宏伟

《机械研究与应用》

DOI

2025

Experimental investigation of evolution characteristics tip flow instability in a centrifugal compressor with a vaneless diffuser

Lei Ming Shi, Hongwei Ma, Rong Jin, Xinghan Yu, Tianyou Wang

Proceedings of the Institution of Mechanical Engineers Part A Journal of Power and Energy

DOI

2024

某离心压气机转子叶尖流场测试及可视化分析

高倩，张一弛，姚峥嵘，马宏伟，郭君德

《测控技术》

2024

A data assimilation pressure field measurement method for linear turbine cascades based on compressed sensing

Yi Yang, Hongwei Ma

Physics of Fluids

DOI

2024

Shock wave structures and vortex unsteadiness in the tip region of a transonic turbine cascade under different conditions

Yi Yang, Hongwei Ma, Anqi Xiao, Lei Ming Shi

Physics of Fluids

DOI

2024

Information transfer between tip leakage vortex and blade aerodynamic force of a compressor cascade

Zengzeng Wang, Hongwei Ma, Yi Yang, Zetao Li

Aerospace Science and Technology

DOI

2024

Analysis of cooling effects and measurement errors in water-cooled thermocouples for total temperature measurement in aviation engine combustion chambers

Qingdian Zhang, Hongwei Ma, Junde Guo, Zetao Li, Anqi Xiao, Yicheng Liu

International Journal of Thermal Sciences

DOI

2024

Study on the influence of pneumatic probe on the wake flow field of transonic turbine cascade

Qingdian Zhang, Hongwei Ma, Anqi Xiao, Yingcun Liu, Junde Guo

Acta Mechanica Sinica

DOI

2024

Effect of Tip Gap Size on the Tip Flow Structure and Turbulence Generation in a Low Reynolds Number Compressor Cascade

Lei Ming Shi, Hongwei Ma, Huajie Wang, Tianyou Wang

Journal of Fluids Engineering

DOI

2024

Investigation of inlet flow influenced on the first rotor flow instability at blade non-synchronous vibration state

Hongwei Ma, Zengzeng Wang, Xiang He, Yafei Zhong

Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering

DOI

2024

Blade aerodynamic force and tip region vortex spatial-temporal evolution study of a compressor cascade

Zengzeng Wang, Hongwei Ma, Yafei Zhong, Yi Yang, Qingdian Zhang

Aerospace Science and Technology

DOI

2023

Spatial-Temporal evolution characteristics of pre-Stage-stall in a centrifugal compressor with a vaneless diffuser and a volute

Lei Ming Shi, Hongwei Ma, Xinghan Yu, Rong Jin, Tianyou Wang

Proceedings of the Institution of Mechanical Engineers Part A Journal of Power and Energy

DOI

2023

Flow structure and vortex dynamics of blade surface transitional flow in the near-tip region of a compressor cascade

Lei Ming Shi, Ruiqing. Mao, Hongwei Ma, Tianyou Wang

Physics of Fluids

DOI

2023

Tip leakage flow of a vibrating airfoil in a linear compressor cascade

Lei Ming Shi, Hongwei Ma, Lixiang Wang, Botao Yu, Tianyou Wang

Physics of Fluids

DOI

2023

Experimental investigation of characteristics and influence of tip leakage vortex wandering in an axial compressor cascade

Lei Ming Shi, Wenxuan Yan, Hongwei Ma, Tianyou Wang

Physics of Fluids

DOI

2023

Manipulating near-wall flow instability and transport characteristics by the airfoil probe: Investigation on a transonic compressor cascade

Qingdian Zhang, Hongwei Ma, Zhongqiang Xie, Zengzeng Wang

Physics of Fluids

DOI

2023

Investigation of tip leakage flow in spatial and temporal scales of axial isolated compressor rotor near stall

Hongwei Ma, Zengzeng Wang, Xiang He, Yafei Zhong

Journal of the Brazilian Society of Mechanical Sciences and Engineering

DOI

2023

Modal Analysis and Vortex Trajectory Description for Tip Leakage Flow of a Transonic Turbine Cascade

Yi Yang, Hongwei Ma, Yafei Zhong, Qingdian Zhang

Journal of Thermal Science

DOI

2023

Effects of the airfoil probes on the aerodynamic performance of a transonic compressor cascade

Qingdian Zhang, Hongwei Ma, Yafei Zhong, Junde Guo, Zhongqiang Xie

Aerospace Science and Technology

DOI

2023

Vortex dynamics and associated turbulence production in the separated transitional flow and the wake at a moderate Reynolds number

Lei Ming Shi, Ruiqing. Mao, Bin Wang, Bin. Wang, Deming Jia, Xuefeng Meng, Wenquan Zhang, Hongwei Ma, Tianyou Wang

Experimental Thermal and Fluid Science

DOI

2022

平面叶栅气动试验研究进展与展望

张庆典，马宏伟，杨益，肖安琪

《力学学报》

2022

组合探针测量压气机级间三维动态流场的方法

马宏伟，贺象，单晓明，姚峥嵘

《航空动力学报》

2022

温升法测量压气机等熵效率的不确定度

马宏伟，李赫

《航空动力学报》

2022

Experimental study on the aerodynamic influence of purge flow in a turbine cascade with different mainstream incidence angles

Lianpeng Zhao, Hongwei Ma

Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering

DOI

2022

Near Field Evolution of Blade Wakes Under the Influence of Upstream Transitional Flow in a Compressor Cascade at Moderate Reynolds Numbers

Lei Ming Shi, Hongwei Ma, Tianyou Wang

Journal of Fluids Engineering

DOI

2022

Analysis of tip leakage flow unsteadiness in a transonic turbine cascade using data-driven modal decomposition methods

Yi Yang, Hongwei Ma

Physics of Fluids

DOI

2022

Hybrid RANS/LES study of tip leakage vortex instability and turbulence characteristics of a transonic turbine cascade

Yi Yang, Hongwei Ma

Aerospace Science and Technology

DOI

2021

轴流涡轮叶尖泄漏流动实验测量技术研究进展

杨益，马宏伟

《实验流体力学》

2021

LDV和PIV测速技术测量离心压气机内部流动的应用进展

尉星航，马宏伟，廖鑫

《实验流体力学》

2021

1.5级燃气轮机上、下游密封系统非定常流动的数值研究（英文）

马宏伟，赵连鹏

《风机技术》

DOI

2021

Numerical study of probe parameters on performance of a transonic axial compressor

Asad Islam, Hongwei Ma

PLoS ONE

DOI

2021

Effects of Probe Stem Surface Suction on the Aerodynamic Performance of a Compressor

Yafei Zhong, Hongwei Ma, Yi Qing Yang

DOI

2020

小尺寸多级轴流压气机级间干扰现象试验

贺象，马宏伟，银越千，单晓明

《航空动力学报》

2020

Application of Phase-Locked PIV Technique to the Measurements of Flow Field in a Turbine Stage

Zhenyang Zhang, Hongwei Ma

Journal of Thermal Science

DOI

2020

Unsteady Analysis of Inlet Hot Streaks Clocking Effects in a 1-1/2 Turbine Stage

Yejia Jin, Hongwei Ma, Xinghang Yu

DOI

2020

POD analysis of the unsteady behavior of blade wake under the influence of laminar separation vortex shedding in a compressor cascade

Lei Ming Shi, Hongwei Ma, Xinghang Yu

Aerospace Science and Technology

DOI

2020

Experimental Investigation of the Effect of Purge Flow and Main Flow Interaction in a Low-Speed Turbine Cascade Passage

Lianpeng Zhao, Hongwei Ma

Entropy

DOI

2020

Numerical Investigation of Probe-Support Intrusion Effects on Transonic Axial Compressor Performance

Asad Islam, Hongwei Ma

International Bhurban Conference on Applied Sciences and Technology (IBCAST)

DOI

2020

Experimental Study on Internal Flow Field of a High-Speed Centrifugal Compressor at Different Altitudes

Xinghang Yu, Hongwei Ma, Lei Ming Shi, Lianpeng Zhao

DOI

2019

Particle Image Velocimetry (PIV) Investigation of Blade and Purge Flow Impacts on Inter-Stage Flow Field in a Research Turbine

Zhenyang Zhang, Hongwei Ma

Energies

DOI

2019

Influence of Probe Measuring Positions on Aerodynamics of a Transonic Axial flow Compressor

Hongwei Ma, Asad Islam

Proceedings

DOI

2019

Analysis of Different POD Processing Methods for SPIV-Measurements in Compressor Cascade Tip Leakage Flow

Lei Ming Shi, Hongwei Ma, Lixiang Wang

Energies

DOI

2019

Effect of Incidence Angle on Entropy Generation in the Boundary Layers on the Blade Suction Surface in a Compressor Cascade

Lei Ming Shi, Hongwei Ma

Entropy

DOI

2018

POD Analysis of Entropy Generation in a Laminar Separation Boundary Layer

Chao Jin, Hongwei Ma

Energies

DOI

2017

An Experimental Investigation of the Effects of Grooved Tip Geometry on the Flow Field in a Turbine Cascade Passage Using Stereoscopic PIV

Yangtao Tian, Hongwei Ma, Lixiang Wang

DOI

2017

Stereoscopic PIV measurements of the flow field in a turbine cascade

Yangtao Tian, Hongwei Ma, Rong Ma

Journal of Thermal Science

DOI

2017

Role of a single shield in thermocouple measurements in hot air flow

Hongwei Ma, Lei Ming Shi, Yangtao Tian

Journal of Thermal Science

DOI

2017

Effects of airfoil-probe tubes on the flow field of a compressor cascade

Hongwei Ma, Chao Jin, Lianpeng Zhao, Rong Ma

Journal of Thermal Science

DOI

2016

小尺寸多级轴流压气机喘振现象试验

贺象，马宏伟，银越千，单晓明，姚峥嵘

《航空动力学报》

2016

探针支杆对压气机转子性能及流场影响的数值模拟研究

马宏伟，项乐

《推进技术》

2016

欠频响压力探针测量压气机动态流场的结果分析

马宏伟，魏巍，张良，官辉

《航空发动机》

2016

低速轴流压气机旋转失速演化机制研究

贺象，银越千，黄生勤，马宏伟，魏巍

《航空发动机》

2016

Experimental Investigation of Effects of Rim Sealing Flow on the Flow Field in a Turbine Cascade Passage With Different Rim Seal Configurations

Lixiang Wang, Hongwei Ma, Jinghui Zhang

DOI

2016

Experimental investigation of flow field in a laboratory-scale compressor

Hongwei Ma, Wei Wei, Xavier Ottavy

Chinese Journal of Aeronautics

DOI

2016

Numerical Investigation of Effects of Non-Uniform Tip Clearance on Flow Field Inside a Turbine Cascade

Hongwei Ma, Yangtao Tian

DOI

2016

Experimental investigation of effects of suction side squealer tip on the aeroelastic stability of a linear oscillating compressor cascade

Hongwei Ma, Chao Jin, Wei Wei

Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering

DOI

2016

Investigation of Tip-leakage-vortex Breakdown and Its Role in Rotating Stall in a 1.5-stage Low-speed Axial-compressor

Xiang He, Hongwei Ma, Wei Wei

HAL (Le Centre pour la Communication Scientifique Directe)

2016

Effects of probe support on the stall characteristics of a low-speed axial compressor

Hongwei Ma, Shaohui Li, Wei Wei

Journal of Thermal Science

DOI

2015

波浪形非均匀间隙封严结构影响涡轮性能的数值模拟

张晶辉，马宏伟

《航空动力学报》

2015

Experimental investigation of effects of suction-side squealer tip geometry on the flow field in a large-scale axial compressor using SPIV

Hongwei Ma, Wei Wei, Lixiang Wang, Yangtao Tian

Journal of Thermal Science

DOI

2015

Experimental study of effects of tip geometry on the flow field in a turbine cascade passage

Hongwei Ma, Lixiang Wang

Journal of Thermal Science

DOI

2014

轮缘封严气体对涡轮转子性能影响的非定常数值研究(英文)

张晶辉，马宏伟

《推进技术》

2014

Effects of probe support on the flow field of a low-speed axial compressor

Hongwei Ma, Shaohui Li, Wei Wei

Journal of Thermal Science

DOI

2013

一种测量跨声速多级压气机转子出口二维流场的方法

马宏伟，贺象，单晓明，姚峥嵘

《推进技术》

2013

Applying low-speed modeling method to high pressure turbine stage

Hongwei Ma

Journal of Aerospace Power

2013

Effects of Blade Tip Geometries on the Aerodynamic Performance of a Compressor Cascade

Hongwei Ma, Jun Zhang, Wei Wei

DOI

2013

Experimental investigation of effects of distributed riblets on aerodynamic performance of a low-speed compressor

Hongwei Ma, Wei Wei

Journal of Thermal Science

DOI

2013

Numerical Investigation of Improving Turbine Sealing Effectiveness Through Slot Width Modification of the Rim Seal

Jinghui Zhang, Hongwei Ma

DOI

2013

Wavelet analysis of the shaft order perturbation and stall inception in an axial compressor

Xiang He, Hongwei Ma, Jun Zhang, Wei Wei

Journal of Thermal Science

DOI

2012

楔顶双孔探针测量跨声多级压气机转子出口三维动态流场的方法

李井洋，马宏伟，贺象

《航空动力学报》

2012

圆柱型两孔针三维流场测试数据处理方法

李井洋，马宏伟

《燃气轮机技术》

2012

Experimental Study of Effects of Grooved Tip Clearances on the Flow Field in a Compressor Cascade Passage

Hongwei Ma, Jun Zhang, Jinghui Zhang, Zhou Yuan

Journal of Turbomachinery

DOI

2012

Numerical Simulation of Effects of Tip Geometry on the Performance of an Axial Compressor

Hongwei Ma, Jun Zhang

ASME Gas Turbine India Conference (GTINDIA)

DOI

2012

Investigation of the Effects of Airfoil-probes on the Aerodynamic Performance of an Axial Compressor

Xiang He, Hongwei Ma, Minglin REN, Honghui Xiang

Chinese Journal of Aeronautics

DOI

2012

Effects of suction side squealer tip on the performance of a low-speed axial compressor

Jun Zhang, Hongwei Ma, Jingyang Li

Journal of Thermal Science

DOI

2011

叶型探针对跨声压气机性能影响的数值模拟

向宏辉，任铭林，马宏伟，贺象

《热能动力工程》

2011

两类叶型探针对扩压叶栅流场影响的对比

向宏辉，任铭林，马宏伟，贺象，姜正礼

《燃气涡轮试验与研究》

2010

叶型探针对压气机叶栅气动性能影响的试验与数值研究

向宏辉，任铭林，马宏伟，贺象，王绍川

《燃气涡轮试验与研究》

2010

Effects of measuring positions on the measured aerodynamic performance of a centrifugal compressor

Hongwei Ma, Jun Zhang

Journal of Thermal Science

DOI

2010

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

Hongwei Ma, Jinghui Zhang, Jun Zhang

Journal of Thermal Science

DOI

2009

进口管道对离心压气机性能影响的数值模拟

张军，马宏伟，何洪，吉建波

《航空动力学报》

2009

利用介质阻挡放电等离子体控制压气机叶栅端壁二次流

李钢，徐燕骥，林彬，王召锋，马宏伟，朱俊强，聂超群

《中国科学:技术科学》

2009

Experimental Study of Effects of Axially Non-Uniform Tip Clearances on the Aerodynamic Performance of a Compressor Cascade

Hongwei Ma, Zhaofeng Wang, Jun Zhang

AIAA Aerospace Sciences Meeting

DOI

2008

叶型探针对轴流压气机性能试验结果的影响

向宏辉，任铭林，马宏伟，黄明镜，樊嘉峰

《燃气涡轮试验与研究》

2008

Effects of a kind of non-smooth blade on the unsteady flow field at the exit of an axial fan

Hongwei Ma, Jibo Guo

Journal of Thermal Science

DOI

2007

非光滑叶片对轴流风扇气动性能的影响

郭继波，马宏伟

《工程热物理学报》

2006

沟槽面对扩压叶栅表面流态的影响

田桥，马宏伟，武卉，高磊

《工程热物理学报》

2006

压气机转子三维流场计算中叶尖间隙网格的影响

张辉，马宏伟，蒋浩康

《航空动力学报》

2006

Effects of a kind of non-smooth blade on the performance of an axial fan

Hongwei Ma, Jibo Guo

Journal of Thermal Science

DOI

2006

Influences of a kind of groove-blade on the flow field in a compressor cascade

Hongwei Ma, Wuying Yan, Qiao Tian

Journal of Thermal Science

DOI

2004

涡轮级轮缘封严内非定常流场的准三维LDV测量

马宏伟，Dieter E Bohn，Achim Decker，Bernd Rudzinski

《航空动力学报》

2002

轴流压气机转子叶尖泄漏涡和尾迹在静子尖区的传播

马宏伟，张庆国，蒋浩康

《工程热物理学报》

2001

轴流压气机小流量状态转子叶尖泄漏涡的三维流动

马宏伟，蒋浩康

《工程热物理学报》

2001

近失速状态轴流压气机转子内尖区三维流动结构

马宏伟，蒋浩康

《工程热物理学报》

2000

从端壁动态压力场看压气机转子尖区流动

马宏伟，蒋浩康

《工程热物理学报》

2000

单转子压气机出口三维流场紊流特性

马宏伟，蒋浩康

《航空动力学报》

2000

离心压气机转子内近端壁区三维紊流流场

马宏伟，蒋浩康，徐月亭，杨健，薛琳

《航空动力学报》

2000

涡轮叶栅端壁区非定常流场显示

马宏伟，蒋浩康，马艳红，曲承魁

《工程热物理学报》

2000

轴流压气机小流量状态转子叶尖泄漏涡三维紊流特性

马宏伟，蒋浩康

《航空动力学报》

2000

压气机转子出口流场的发展及三维紊流特性

马宏伟，蒋浩康

《航空动力学报》

2000

单转子轴流压气机不同状态下进出口三维时均流场

马宏伟，蒋浩康，董玉玺

《航空动力学报》

1999

轴流压气机转子尖区三维紊流特性

马宏伟，蒋浩康，叶大均，徐纲，赵全春，董玉玺

《工程热物理学报》

1999

叶轮出口总温总压测量用单热膜吸气探针的研究

蒋浩康，王洪伟，马宏伟

《工程热物理学报》

1999

多级离心压缩机械的系统稳定性分析

聂超群，蒋浩康，王维琮，马宏伟，何少伟，陈静宜

《工程热物理学报》

1998

压气机设计状态转子出口及下游三维紊流流场

马宏伟，蒋浩康

《燃气涡轮试验与研究》

1998

轴流风机转子通道内尖区三维流场

马宏伟，蒋浩康，聂超群

《工程热物理学报》

1998

轴流压气机时尖泄漏涡的时均流动

马宏伟，蒋浩康，叶大均，徐纲，赵全春，董玉玺

《工程热物理学报》

1998

压气机转子三维紊流流场

蒋浩康，马宏伟

《工程热物理学报》

1997

单转子压气机设计状态和近失速状态出口三维紊流流场

马宏伟，蒋浩康

《工程热物理学报》

1997

压气机转子尾迹三维紊流特性分析

马宏伟，蒋浩康

《工程热物理学报》

1997

速度梯度和近壁效应对压力探针测量误差的影响

马宏伟，蒋浩康

《燃气涡轮试验与研究》

1997

压气机转子通道内尖区三维平均流场

马宏伟，蒋浩康

《航空动力学报》

1997

压气机不同状态下转子出口三维紊流流场

马宏伟，蒋浩康

《航空动力学报》

精选作品

期刊论文

大尺寸多功能涡轮试验装置及测试系统

Research on error analysis and compensation method of combined water-cooled rake for enhanced temperature measurement accuracy

低速轴流压气机叶尖泄漏涡破碎研究

Experimental investigation of evolution characteristics tip flow instability in a centrifugal compressor with a vaneless diffuser

某离心压气机转子叶尖流场测试及可视化分析

A data assimilation pressure field measurement method for linear turbine cascades based on compressed sensing

Shock wave structures and vortex unsteadiness in the tip region of a transonic turbine cascade under different conditions

Information transfer between tip leakage vortex and blade aerodynamic force of a compressor cascade

Analysis of cooling effects and measurement errors in water-cooled thermocouples for total temperature measurement in aviation engine combustion chambers

Study on the influence of pneumatic probe on the wake flow field of transonic turbine cascade

Effect of Tip Gap Size on the Tip Flow Structure and Turbulence Generation in a Low Reynolds Number Compressor Cascade

Investigation of inlet flow influenced on the first rotor flow instability at blade non-synchronous vibration state

Blade aerodynamic force and tip region vortex spatial-temporal evolution study of a compressor cascade

Spatial-Temporal evolution characteristics of pre-Stage-stall in a centrifugal compressor with a vaneless diffuser and a volute

Flow structure and vortex dynamics of blade surface transitional flow in the near-tip region of a compressor cascade

Tip leakage flow of a vibrating airfoil in a linear compressor cascade

Experimental investigation of characteristics and influence of tip leakage vortex wandering in an axial compressor cascade

Manipulating near-wall flow instability and transport characteristics by the airfoil probe: Investigation on a transonic compressor cascade

Investigation of tip leakage flow in spatial and temporal scales of axial isolated compressor rotor near stall

Modal Analysis and Vortex Trajectory Description for Tip Leakage Flow of a Transonic Turbine Cascade

Effects of the airfoil probes on the aerodynamic performance of a transonic compressor cascade

Vortex dynamics and associated turbulence production in the separated transitional flow and the wake at a moderate Reynolds number

平面叶栅气动试验研究进展与展望

组合探针测量压气机级间三维动态流场的方法

温升法测量压气机等熵效率的不确定度

Experimental study on the aerodynamic influence of purge flow in a turbine cascade with different mainstream incidence angles

Near Field Evolution of Blade Wakes Under the Influence of Upstream Transitional Flow in a Compressor Cascade at Moderate Reynolds Numbers

Analysis of tip leakage flow unsteadiness in a transonic turbine cascade using data-driven modal decomposition methods

Hybrid RANS/LES study of tip leakage vortex instability and turbulence characteristics of a transonic turbine cascade

轴流涡轮叶尖泄漏流动实验测量技术研究进展

LDV和PIV测速技术测量离心压气机内部流动的应用进展

1.5级燃气轮机上、下游密封系统非定常流动的数值研究（英文）

Numerical study of probe parameters on performance of a transonic axial compressor

Effects of Probe Stem Surface Suction on the Aerodynamic Performance of a Compressor

小尺寸多级轴流压气机级间干扰现象试验

Application of Phase-Locked PIV Technique to the Measurements of Flow Field in a Turbine Stage

Unsteady Analysis of Inlet Hot Streaks Clocking Effects in a 1-1/2 Turbine Stage

POD analysis of the unsteady behavior of blade wake under the influence of laminar separation vortex shedding in a compressor cascade

Experimental Investigation of the Effect of Purge Flow and Main Flow Interaction in a Low-Speed Turbine Cascade Passage

Numerical Investigation of Probe-Support Intrusion Effects on Transonic Axial Compressor Performance

Experimental Study on Internal Flow Field of a High-Speed Centrifugal Compressor at Different Altitudes

Particle Image Velocimetry (PIV) Investigation of Blade and Purge Flow Impacts on Inter-Stage Flow Field in a Research Turbine

Influence of Probe Measuring Positions on Aerodynamics of a Transonic Axial flow Compressor

Analysis of Different POD Processing Methods for SPIV-Measurements in Compressor Cascade Tip Leakage Flow

Effect of Incidence Angle on Entropy Generation in the Boundary Layers on the Blade Suction Surface in a Compressor Cascade

POD Analysis of Entropy Generation in a Laminar Separation Boundary Layer

An Experimental Investigation of the Effects of Grooved Tip Geometry on the Flow Field in a Turbine Cascade Passage Using Stereoscopic PIV

Stereoscopic PIV measurements of the flow field in a turbine cascade

Role of a single shield in thermocouple measurements in hot air flow

Effects of airfoil-probe tubes on the flow field of a compressor cascade

小尺寸多级轴流压气机喘振现象试验

探针支杆对压气机转子性能及流场影响的数值模拟研究

欠频响压力探针测量压气机动态流场的结果分析

低速轴流压气机旋转失速演化机制研究

Experimental Investigation of Effects of Rim Sealing Flow on the Flow Field in a Turbine Cascade Passage With Different Rim Seal Configurations

Experimental investigation of flow field in a laboratory-scale compressor

Numerical Investigation of Effects of Non-Uniform Tip Clearance on Flow Field Inside a Turbine Cascade

Experimental investigation of effects of suction side squealer tip on the aeroelastic stability of a linear oscillating compressor cascade

Investigation of Tip-leakage-vortex Breakdown and Its Role in Rotating Stall in a 1.5-stage Low-speed Axial-compressor

Effects of probe support on the stall characteristics of a low-speed axial compressor

波浪形非均匀间隙封严结构影响涡轮性能的数值模拟

Experimental investigation of effects of suction-side squealer tip geometry on the flow field in a large-scale axial compressor using SPIV

Experimental study of effects of tip geometry on the flow field in a turbine cascade passage

轮缘封严气体对涡轮转子性能影响的非定常数值研究(英文)

Effects of probe support on the flow field of a low-speed axial compressor

一种测量跨声速多级压气机转子出口二维流场的方法

Applying low-speed modeling method to high pressure turbine stage

Effects of Blade Tip Geometries on the Aerodynamic Performance of a Compressor Cascade

Experimental investigation of effects of distributed riblets on aerodynamic performance of a low-speed compressor

Numerical Investigation of Improving Turbine Sealing Effectiveness Through Slot Width Modification of the Rim Seal

Wavelet analysis of the shaft order perturbation and stall inception in an axial compressor

楔顶双孔探针测量跨声多级压气机转子出口三维动态流场的方法

圆柱型两孔针三维流场测试数据处理方法

Experimental Study of Effects of Grooved Tip Clearances on the Flow Field in a Compressor Cascade Passage

Numerical Simulation of Effects of Tip Geometry on the Performance of an Axial Compressor

Investigation of the Effects of Airfoil-probes on the Aerodynamic Performance of an Axial Compressor

Effects of suction side squealer tip on the performance of a low-speed axial compressor

叶型探针对跨声压气机性能影响的数值模拟