鹿哈男｜北京航空航天大学｜学者主页

2026

A low-loss power matching method for gas turbine based on downstream free turbine guide vane re-design in a turboprop engine

Chi Liu, Hanan Lu, Xin Tang, Chongxin Zhang, Qiushi Li

Proceedings of the Institution of Mechanical Engineers Part C Journal of Mechanical Engineering Science

DOI

2026

Adversarial Feature Fusion Network for Aeropropulsion Fan Design Space Mapping

Tao Ma, Wei Yuan, Hanan Lu, Qiushi Li

AIAA Journal

DOI

2026

Investigations on the flow separation characteristics and control strategy in a conical diffuser with skewed struts of symmetric airfoils

Weizhe Feng, Hanan Lu, Ziwan Li

Aerospace Science and Technology

DOI

2025

鼓包唇口对边界层抽吸涵道风扇的性能影响及作用机理研究

王磊，苏冠廷，潘天宇，鹿哈男，郑孟宗，李秋实

《推进技术》

2025

Numerical investigation of the flow characteristics in a semicircular S-shape inlet duct with large offset for boundary layer ingestion propulsion system

Hanan Lu, Haoran Li, Lei Wang, Qiushi Li

Physics of Fluids

DOI

2025

An efficient aerodynamic modeling method based on micro-element partitioning sampling and adaptive data fusion

Lei Wang, Hanan Lu, Dongsheng Gong, Qiushi Li

Physics of Fluids

DOI

2025

A data-driven tip flow loss prediction model for a boundary layer ingesting fan based on a dataset generated under uniform inflow conditions

Kaikai Shi, Hanan Lu, Yixuan Wang, Shaofeng Xu, Zhibo Sun, Yanxia Niu, Lei Li, Yan Shi

Science China Technological Sciences

DOI

2025

A systematic review of boundary layer ingestion (BLI) fan: Current Status and future perspectives

Tao Ma, Hanan Lu, Qiushi Li

Progress in Aerospace Sciences

DOI

2025

A loss reduction design strategy for a ducted fan under boundary layer ingestion condition based on a lip bump

Hanan Lu, Lei Wang, Guanting Su, Qiushi Li

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

DOI

2025

Load-oriented aerodynamic design approach of low-speed axial fans in the preliminary design stage

Tao Ma, Hanan Lu, Li Qiushi

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

DOI

2024

An efficient cooling design strategy for the embedded driving motor under the hub by using the high-pressure airflow after the rotor in an electrical ducted fan system

Xin Tang, Hanan Lu, Lei Wang, Qiushi Li

Aerospace Science and Technology

DOI

2024

Influences of radial migration flow on the compressor stage losses under low Reynolds number conditions

Shuqiu Zhang, Hanan Lu, Qiushi Li

Physics of Fluids

DOI

2024

Optimization design method based on parameter reduction and active subspaces: Redistribution of chordwise loading at blade tips in a transonic axial-flow fan

Tao Ma, Hanan Lu, Qiushi Li

Physics of Fluids

DOI

2024

Impact of circumferential inlet distortion on different types of stall inceptions in a transonic compressor

Tianyu Pan, Jiandong Yan, Hanan Lu, Qiushi Li

Chinese Journal of Aeronautics

DOI

2023

基于物理嵌入神经网络的叶栅损失模型

冯云阳，宋西镇，袁巍，鹿哈男

《航空动力学报》

2023

基于数据驱动的复杂进气下风扇转子叶根损失模型

石凯凯，鹿哈男，潘天宇，李秋实

《航空动力学报》

2023

A region-segmentation combinational loss model based on data-driven machine learning for a boundary layer ingestion fan

Tianyu Pan, Kaikai Shi, Hanan Lu, Zhe Yang, Jian Zhang, Qiushi Li

Aerospace Science and Technology

DOI

2023

A data-driven flow loss prediction model for the blade hub region of a boundary layer ingestion fan rotor

Kaikai Shi, Hanan Lu, Xizhen Song, Tianyu Pan, Zhe Yang, Jian Zhang, Qiushi Li

International Journal of Numerical Methods for Heat &amp Fluid Flow

DOI

2023

An efficient flow control technique based on co-flow jet and multi-stage slot circulation control applied to a supercritical airfoil

Lei Wang, Hanan Lu, Yue Xu, Qiushi Li

International Journal of Turbo and Jet Engines

DOI

2023

Physics-informed deep learning cascade loss model

Yunyang Feng, Xizhen Song, Wei Yuan, Hanan Lu

Aerospace Science and Technology

DOI

2022

Forced Response Induced by Low Engine Order Under Circumferential Inlet Distortions With Different Extents

Tianyu Pan, Zhaoqi Yan, Hanan Lu, Qiushi Li, Robert E. Kielb

Journal of Turbomachinery

DOI

2022

A Data-Driven Tip Flow Loss Prediction Method for a Transonic Fan Under Boundary Layer Ingesting Inflow Distortion

Zhe Yang, Hanan Lu, Tianyu Pan, Qiushi Li

Journal of Turbomachinery

DOI

2022

Numerical Investigations of a Non-Uniform Stator Dihedral Design Strategy for a Boundary Layer Ingestion (BLI) Fan

Tianyu Pan, Kaikai Shi, Hanan Lu, Zhiping Li, Jian Zhang

Energies

DOI

2022

Numerical study on rotor tip flow loss in a boundary layer ingesting fan under different operating conditions

Hanan Lu, Zhe Yang, Tianyu Pan, Qiushi Li

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

DOI

2021

Numerical Investigation on the Influences of Boundary Layer Ingestion on Tip Leakage Flow Structures and Losses in a Transonic Axial-Flow Fan

Zhe Yang, Hanan Lu, Tianyu Pan, Qiushi Li

Journal of Fluids Engineering

DOI

2021

Numerical investigation on the forced vibration induced by the low engine order under boundary layer ingestion condition

Tianyu Pan, Zhaoqi Yan, Hanan Lu, Qiushi Li

Aerospace Science and Technology

DOI

2020

风车状态下转子性能及通道内流动分析

李达，鹿哈男，潘天宇，李秋实

《航空动力学报》

DOI

2020

Optimization of a transonic axial-flow compressor under inlet total pressure distortion to enhance aerodynamic performance

Da Li, Hanan Lu, Zhe Yang, Tianyu Pan, Hai Du, Li Qiushi

Engineering Applications of Computational Fluid Mechanics

DOI

2019

进气畸变下风扇叶型多目标优化（英文）

陈梦羽，鹿哈男，潘天宇，李秋实

《风机技术》

DOI

2019

An adaptive region segmentation combining surrogate model applied to correlate design variables and performance parameters in a transonic axial compressor

Hanan Lu, Qiushi Li, Tianyu Pan, Ramesh K. Agarwal

Engineering With Computers

DOI

2019

Analysis and application of shroud wall optimization to an axial compressor with upstream boundary layer to improve aerodynamic performance

Hanan Lu, Qiushi Li, Tianyu Pan, Ramesh K. Agarwal

International Journal of Numerical Methods for Heat &amp Fluid Flow

DOI

2019

Non-uniform stator loss reduction design strategy in a transonic axial-flow compressor stage under inflow distortion

Hanan Lu, Zhe Yang, Tianyu Pan, Qiushi Li

Aerospace Science and Technology

DOI

2018

Optimization strategy for a single-stage axisymmetric hub endwall in axial compressor by a modified transonic area rule

Zhiping Li, Yafei Zhang, Tianyu Pan, Hanan Lu, Miao Wu, Jian Zhang

Aerospace Science and Technology

DOI

2018

Optimization Strategy for an Axial-Flow Compressor Using a Region-Segmentation Combining Surrogate Model

Hanan Lu, Qiushi Li, Tianyu Pan

Journal of Aerospace Engineering

DOI

2018

Using forward end-sweep to reduce transonic cantilevered stator losses to improve compressor performance

Hanan Lu, Qiushi Li, Tianyu Pan

Engineering Applications of Computational Fluid Mechanics

DOI

2017

局部端前掠对跨音悬臂静子气动性能影响研究

鹿哈男，李秋实，潘天宇

《工程热物理学报》

2017

Development of a coupled supersonic inlet-fan Navier–Stokes simulation method

Qiushi Li, Yongzhao LYU, Tianyu Pan, Da Li, Hanan Lu, Yifang Gong

Chinese Journal of Aeronautics

DOI

2017

Effects of axisymmetric arc-shaped slot casing treatment on partial surge initiated instability in a transonic axial flow compressor

Tianyu Pan, Qiushi Li, Yuan Wei, Hanan Lu

Aerospace Science and Technology

DOI

2015

An Integrated Optimization Design Method Based on Surrogate Modeling Applied to Diverging Duct Design

Hanan Lu, Qiushi Li, Shaobin Li

International Journal of Turbo and Jet Engines

DOI

2014

A combinatorial optimization design method applied to S-shaped compressor transition duct design

Hanan Lu, Xinqian Zheng, Qiushi Li

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

DOI

精选作品

期刊论文

A low-loss power matching method for gas turbine based on downstream free turbine guide vane re-design in a turboprop engine

Adversarial Feature Fusion Network for Aeropropulsion Fan Design Space Mapping

Investigations on the flow separation characteristics and control strategy in a conical diffuser with skewed struts of symmetric airfoils

鼓包唇口对边界层抽吸涵道风扇的性能影响及作用机理研究

Numerical investigation of the flow characteristics in a semicircular S-shape inlet duct with large offset for boundary layer ingestion propulsion system

An efficient aerodynamic modeling method based on micro-element partitioning sampling and adaptive data fusion

A data-driven tip flow loss prediction model for a boundary layer ingesting fan based on a dataset generated under uniform inflow conditions

A systematic review of boundary layer ingestion (BLI) fan: Current Status and future perspectives

A loss reduction design strategy for a ducted fan under boundary layer ingestion condition based on a lip bump

Load-oriented aerodynamic design approach of low-speed axial fans in the preliminary design stage

An efficient cooling design strategy for the embedded driving motor under the hub by using the high-pressure airflow after the rotor in an electrical ducted fan system

Influences of radial migration flow on the compressor stage losses under low Reynolds number conditions

Optimization design method based on parameter reduction and active subspaces: Redistribution of chordwise loading at blade tips in a transonic axial-flow fan

Impact of circumferential inlet distortion on different types of stall inceptions in a transonic compressor

基于物理嵌入神经网络的叶栅损失模型

基于数据驱动的复杂进气下风扇转子叶根损失模型

A region-segmentation combinational loss model based on data-driven machine learning for a boundary layer ingestion fan

A data-driven flow loss prediction model for the blade hub region of a boundary layer ingestion fan rotor

An efficient flow control technique based on co-flow jet and multi-stage slot circulation control applied to a supercritical airfoil

Physics-informed deep learning cascade loss model

Forced Response Induced by Low Engine Order Under Circumferential Inlet Distortions With Different Extents

A Data-Driven Tip Flow Loss Prediction Method for a Transonic Fan Under Boundary Layer Ingesting Inflow Distortion

Numerical Investigations of a Non-Uniform Stator Dihedral Design Strategy for a Boundary Layer Ingestion (BLI) Fan

Numerical study on rotor tip flow loss in a boundary layer ingesting fan under different operating conditions

Numerical Investigation on the Influences of Boundary Layer Ingestion on Tip Leakage Flow Structures and Losses in a Transonic Axial-Flow Fan

Numerical investigation on the forced vibration induced by the low engine order under boundary layer ingestion condition

风车状态下转子性能及通道内流动分析

Optimization of a transonic axial-flow compressor under inlet total pressure distortion to enhance aerodynamic performance

进气畸变下风扇叶型多目标优化（英文）

An adaptive region segmentation combining surrogate model applied to correlate design variables and performance parameters in a transonic axial compressor

Analysis and application of shroud wall optimization to an axial compressor with upstream boundary layer to improve aerodynamic performance

Non-uniform stator loss reduction design strategy in a transonic axial-flow compressor stage under inflow distortion

Optimization strategy for a single-stage axisymmetric hub endwall in axial compressor by a modified transonic area rule

Optimization Strategy for an Axial-Flow Compressor Using a Region-Segmentation Combining Surrogate Model

Using forward end-sweep to reduce transonic cantilevered stator losses to improve compressor performance

局部端前掠对跨音悬臂静子气动性能影响研究

Development of a coupled supersonic inlet-fan Navier–Stokes simulation method

Effects of axisymmetric arc-shaped slot casing treatment on partial surge initiated instability in a transonic axial flow compressor

An Integrated Optimization Design Method Based on Surrogate Modeling Applied to Diverging Duct Design

A combinatorial optimization design method applied to S-shaped compressor transition duct design

研究方向