Min Li, Xiaochen Mao, Wenjie Wang, Limin Gao, Bo Liu (2026). Effects of speed matching on the performance and flow characteristics of a counter-rotating axial-flow compressor under inlet distortion. Aerospace Science and Technology.DOI
Lei Wang, Jun Zhang, Hang Shi, Limin Gao, Xiaochen Mao (2026). Exploration and application of the endoscopic pressure-sensitive paint measurement method in confined compressor cascade environments. Aerospace Science and Technology.DOI
Chi Ma, Ruiyu Li, Kexin Wu, Yang Wang, Ziyu Zhao, Limin Gao (2026). Influence of Uncertain Inflow Conditions in Flight Tests on Aerodynamic Performance of a Transonic Compressor Rotor. Journal of Thermal Science.DOI
Bin Zhang (64682), Yunuo Xu, Fei Zhao, Jihong Zhu, Xuanyan Lu, Jinrui Cui, Limin Gao, Zhifeng Zhang, Xu Long (2026). Multi-scale topology optimization of hybrid porous heat sinks using multiple lattice configurations. International Journal of Heat and Mass Transfer.DOI
Limin Gao, Yue Dan, H. D. Wang, Ruiyu Li, Guang Yang (2026). A dataset of measured machining deviations of compressor rotor blades. Scientific Data.DOI
Kaixun Jia, Bin Zhang, Yunuo Xu, Fei Zhao, Jihong Zhu, Limin Gao, Zhifeng Zhang, Xuanyan Lu, Chengbo Ma, Xu Long (2026). Multilayer topology optimization of microfluidic heat sinks using non-Newtonian fluid for electronics cooling. Applied Mathematical Modelling.DOI
Lingsong Fan, Yun Zhu, Kunhao Wu, Ying Zhang, Li-Min Gao, Bao-Hai Wu (2026). A geometry-constraint-driven high-precision cutter contact point determination method for toroidal end mills in five-axis machining of compressor blades. Aerospace Science and Technology.DOI
Chi Ma, Ruiyu Li, Limin Gao, Yang Wang (2025). Influence of Uncertain Inflow Condition of Altitude Simulated Test Facility on Aerodynamic Performance of Compressor Blade. Lecture notes in mechanical engineering.DOI
Yue Dan, Limin Gao, Yuyang HAO, Qiusheng LUO, Ruiyu Li, Guang Yang (2025). Statistical characteristics mining of measured machining error of multi-stage compressor blisks. Chinese Journal of Aeronautics.DOI
Fei Chen, Xiaochen Mao, Lei Fu, Limin Gao, Bo Liu (2025). Stall analysis based on reduced-order variational mode decomposition for a counter-rotating axial compressor. Proceedings.DOI
Limin Gao, Panpan Tu, Guang Cheng Yang, Yang Song (2025). Uncertainty Modeling of Fouling Thickness and Morphology on Compressor Blade. Aerospace.DOI
Yanchao Guo, Yawei Liu, Ke Wang, Ning Ge, Ruiyu Li, Limin Gao (2025). Experimental investigation on the flow instability mechanism for a counter-rotating axial compressor. Aerospace Science and Technology.DOI
Yanchao Guo, Yawei Liu, Lei Wang, Limin Gao, Xiaochen Mao, Ruiyu Li (2025). Experimental and numerical study on stability enhancement casing treatment in a counter-rotating axial compressor. Aerospace Science and Technology.DOI
Panpan Tu, Guang Yang, Limin Gao, Tantao Liu, Song Yang (2025). Uncertainty effect of leading edge fouling on aerodynamic performance of compressor cascades. Aerospace Science and Technology.DOI
Guang Yang, Limin Gao, Panpan Tu, Yue Dan (2025). Effects of uniform profile tolerance on aerodynamic performance eligibility of high subsonic cascade. Aerospace Science and Technology.DOI
Rui-Yu Li, Wei-Qi Tang, Li-Min Gao, Ming Cai (2025). Assessment of numerical uncertainty in compressor cascade CFD validation: effects of blade models with and without axial velocity density ratio (AVDR). Proceedings of Global Power & Propulsion Society.DOI
Li-Min Gao, Guang Yang, Yue Dan, Panpan Tu, Rui-Yu Li (2025). Non-uniform profile tolerance design of a high subsonic cascade based on aerodynamic performance eligibility. Proceedings of Global Power & Propulsion Society.DOI
Yue Dan, Li-Min Gao, Guang Yang, Rui-Yu Li, Haohao Wang (2025). Study on Aerodynamic Effect of Leading-Edge Radius Error and Tolerance Design Considering Compressor Airfoil Size Characteristic. 2025 International Conference of Mechanical Engineering on Aerospace (CoMEA).DOI
Guanzhong Ma, Shiyan Lin, Rui-Yu Li, Li-Min Gao (2025). Spatial Compressed Spectral Proper Orthogonal Decomposition based on Spectrum Translation Property. Proceedings of Global Power & Propulsion Society.DOI
Li-Min Gao, Hanyu Deng, Xue-Song Ni, Yuyang Luo, Yan-Bo Chen (2025). Research on Collaborative Optimization of Pressure and Temperature in Advanced Adiabatic Compressed Air Energy Storage System. 2025 7th International Conference on Power and Energy Technology (ICPET).DOI
Lei Wang, Xiaochen Mao, Guanzhong Ma, Yawei Liu, Limin Gao (2024). Investigation of unsteady characteristics in a counter-rotating compressor based on unsteady numerical simulation and mode decomposition methods. Aerospace Science and Technology.DOI
T. Liu, Limin Gao, Ruiyu Li (2024). Experimental Data-Driven Flow Field Prediction for Compressor Cascade based on Deep Learning and ℓ1 Regularization. Journal of Thermal Science.DOI
Lingsong Fan, Yubin Ren, Miaolong Tan, Baohai Wu, Limin Gao (2024). Exploratory Factor Analysis for Machining Error Data of Compressor Blades Based on Dimensionality-Reduced Statistical Analysis Method. Journal of Manufacturing Science and Engineering.DOI
Yue Dan, Ruiyu Li, Limin Gao, Huawei Yu, Yuyang Hao (2024). Twist Angle Error Statistical Analysis and Uncertain Influence on Aerodynamic Performance of Three-Dimensional Compressor Rotor. Aerospace.DOI
Xiaoxu Kan, Haodong Lei, Limin Gao, Wanyang Wu, Jingjun Zhong (2024). A parametric approach to flow loss with incidence and tip clearance variables for a compressor linear cascade. Physics of Fluids.DOI
Shiyan Lin, Ruiyu Li, Limin Gao (2024). Dynamic Characteristics of the Tip Clearance Flow Based on the Leakage Flow Model.DOI
Haohao Wang, Limin Gao, Guang Cheng Yang, Ruiyu Li, Baohai Wu (2024). A Preconditioner-Based Data-Driven Polynomial Expansion Method: Application to Compressor Blade With Leading Edge Uncertainty. Journal of Engineering for Gas Turbines and Power.DOI
Lingsong Fan, Yubin Ren, Miaolong Tan, Baohai Wu, Limin Gao (2024). GA-BP neural network-based nonlinear regression model for machining errors of compressor blades. Aerospace Science and Technology.DOI
Shiyan Lin, Ruiyu Li, Limin Gao (2024). Study on the Tip Leakage Loss Mechanism of a Compressor Cascade Using the Enhanced Delay Detached Eddy Simulation Method. Entropy.DOI
Haohao Wang, Limin Gao, Guang Yang, Baohai Wu (2024). A data-driven polynomial chaos method for uncertainty quantification of a subsonic compressor cascade with stagger angle errors. Proceedings of the Institution of Mechanical Engineers Part A Journal of Power and Energy.DOI
Ruiyu Li, Limin Gao, Shiyan Lin, Ning Ge (2024). Experimental investigations of dominant unsteady surface pressure in the corner separation region of a high-subsonic compressor cascade. Physics of Fluids.DOI
Xiangfu Lei, Limin Gao, Longrui Chang, Guanhua Yang, Xiaochen Mao (2024). Application of Pressure-Sensitive Paint Measurement Technology in Pressure Measurement of Cascade Blade Surface. Springer proceedings in physics.DOI
Lingsong Fan, Guang Yang, Ying Zhang, Li-Min Gao, Bao-Hai Wu (2024). A novel tolerance optimization approach for compressor blades: incorporating the measured out-of-tolerance error data and aerodynamic performance. Aerospace Science and Technology.DOI
Da-Peng Zhang, Cameron Tropea, Wu Zhou, Tian-Yi Cai, Hao-Qin Huang, Xiangrui Dong, Li-Min Gao, Xiaoshu Cai (2024). Particle streak velocimetry: a review. Experiments in Fluids.DOI
Duan-Yu Zhang, Hao-Qin Huang, Wu Zhou, Ming-Jun Feng, Da-Peng Zhang, Li-Min Gao (2024). Reconstruction of particle distribution for tomographic particle image velocimetry based on unsupervised learning method. Particuology.DOI
Shiyan Lin, Ruiyu Li, Limin Gao, Ning Ge (2023). Accuracy Investigations of Dynamic Characteristic Predictions of Tip Leakage Flow Using Detached Eddy Simulation. Aerospace.DOI
Haohao Wang, Limin Gao, Baohai Wu (2023). Critical Sample-Size Analysis for Uncertainty Aerodynamic Evaluation of Compressor Blades with Stagger-Angle Errors. Aerospace.DOI
Yanchao Guo, Limin Gao, Xiaochen Mao, Chi Ma, Guanzhong Ma (2023). Dynamic mode decomposition for the tip unsteady flow analysis in a counter-rotating axial compressor. Physics of Fluids.DOI
Ruiyu Li, Shiyan Lin, Ning Ge, Limin Gao (2023). Nonembedded measurement method based on amplitude correction for unsteady surface pressure estimation in a high-subsonic compressor cascade. Measurement.DOI
Haohao Wang, Limin Gao, Guang Yang, Baohai Wu (2023). A data-driven robust design optimization method and its application in compressor blade. Physics of Fluids.DOI
Ning Ge, Ruiyu Li, Limin Gao, Lei Wang, Bo Ouyang (2023). An accumulated imaging method with phase-locking for rotor pressure-sensitive paint measurements. Experiments in Fluids.DOI
Lei Wang, Xiaochen Mao, Limin Gao, Yanchao Guo, Yibo Yu (2023). Effect of axial slot casing treatment on the flow instability for different speed ratios in a counter-rotating axial flow compressor. Aerospace Science and Technology.DOI
Jianing Dang, Baohai Wu, Ying Zhang, Limin Gao (2023). A model reconstruction strategy with geometric parameters adjustment function for repairing damaged blade. The International Journal of Advanced Manufacturing Technology.DOI
Yanchao Guo, Xiaochen Mao, Limin Gao (2023). Numerical investigation on the cross-stage self-recirculating casing treatment for a counter-rotating axial compressor. Aerospace Science and Technology.DOI
Bin Zhang, Jihong Zhu, Longfei Gong, Kaixun Jia, Limin Gao (2023). Topology optimization of heat sink in turbulent natural convection using k-ω turbulent model. Applied Mathematical Modelling.DOI
Yanchao Guo, Limin Gao, Xiaochen Mao (2022). Effect of self-recirculating casing treatment on the unsteady flow and stability of counter-rotating axial-flow compressor. International Journal of Turbo and Jet Engines.DOI
Yanchao Guo, Xiaochen Mao, Lei Wang, Limin Gao (2022). Effect of axial slot casing treatment on a counter-rotating axial-flow compressor aerodynamic performance and stability. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering.DOI
Guanhua Yang, Limin Gao, Haohao Wang, Longrui Chang (2022). Influence of leading edge point on aerodynamic performance of asymmetric leading edge compressor airfoils. International Journal of Turbo and Jet Engines.DOI
Guanhua Yang, Limin Gao, Tianyu Gao, Yanchao Guo (2022). Application of pre-positioning method in compressor cascade measurement with pressure-sensitive paint. Measurement Science and Technology.DOI
Yanchao Guo, Xiaochen Mao, Limin Gao, Yibo Yu (2022). Numerical study on the stability enhancement mechanism of self-recirculating casing treatment in a counter-rotating axial-flow compressor. Engineering Applications of Computational Fluid Mechanics.DOI
Limin Gao, Chi Ma, Ming Cai, Ruiyu Li, Haohao Wang, Guang Yang (2022). Influence of uncertain inflow conditions on a subsonic compressor cascade based on wind tunnel experiment. Proceedings of the Institution of Mechanical Engineers Part C Journal of Mechanical Engineering Science.DOI
Tantao Liu Tantao Liu, Limin Gao, Xudong Feng (2022). Research of laws and prediction of axial-flow compressor characteristics based on data driven. Proceedings.DOI
Yanchao Guo, Limin Gao, Lei WANG, Xiaochen Mao (2022). Effect of axial slot casing treatment on a counter-rotating axial compressor performance and stability. Proceedings.DOI
Zhiyuan Cao, Xiang Zhang, Chuxuan Wang, Xi Gao, Limin Gao, Бо Лю (2022). A study on the flow physics of a supersonic partial admission impulse turbine for different tip clearances. Aerospace Science and Technology.DOI
Ming Cai, Limin Gao, Haoxue Li, Yangbo Ou (2022). Flow quality improvement of the wind tunnel testing for a highly-loaded compressor cascade at high incidence. International Journal of Turbo and Jet Engines.DOI
Ruiyu Li, Lei Zhao, Ning Ge, Limin Gao, Ming‐Jiu Ni (2022). Grid resolution assessment method for hybrid RANS-LES in turbomachinery. Engineering Applications of Computational Fluid Mechanics.DOI
Limin Gao, Guanhua Yang, Tianyu Gao, Ruiyu Li, Xiaoquan Hu (2021). Experimental Investigation of a Linear Cascade with Large Solidity Using Pressure Sensitive Paint and Dual-Camera System. Journal of Thermal Science.DOI
Yun Shao, Liusheng Chen, Qi Liao, Heng Jiang, Zhitian Liu, Xigao Jin, Limin Gao (2020). Characterization of Response Frequency for the Pressure-Sensitive Paint Based on Fluorine-Containing Polymer Matrixes Using Oscillating Sound Wave Technique. Sensors.DOI
Haohao Wang, Lei Zhao, Limin Gao, Yongzeng Li, Chi Ma (2020). Influence of Blade Tip Fillet Structure on Aerodynamic Performance of a Compressor Rotor.DOI
Chi Ma, Limin Gao, Haohao Wang, Ruiyu Li, Baohai Wu (2020). Influence of leading edge with real manufacturing error on aerodynamic performance of high subsonic compressor cascades. Chinese Journal of Aeronautics.DOI
Feng Wu, Limin Gao, Lu Gang Yang, Aqiang Lin, Hai Zhang (2020). Numerical Analysis of High-Altitude Inlet Air on Boundary Layer Flow Loss in an Aero-Engine Compressor. Energies.DOI
Zhiyuan Cao, Cheng Song, Bo Liu, Limin Gao (2020). Influence of endwall slotted injection on performance and flow physics in a compressor cascade. Proceedings of the Institution of Mechanical Engineers Part A Journal of Power and Energy.DOI
Bin Zhang, Jihong Zhu, Gaoxiang Xiang, Limin Gao (2020). Design of nanofluid-cooled heat sink using topology optimization. Chinese Journal of Aeronautics.DOI
Bin Zhang, Jihong Zhu, Limin Gao (2020). Topology optimization design of nanofluid-cooled microchannel heat sink with temperature-dependent fluid properties. Applied Thermal Engineering.DOI
Ruiyu Li, Limin Gao, Chi Ma, Shiyan Lin, Lei Zhao (2020). Corner separation dynamics in a high-speed compressor cascade based on detached-eddy simulation. Aerospace Science and Technology.DOI
Feng Wu, Limin Gao, Xin-Yun Wu, Xudong Feng, Lintao Leng, Yaoyu Li (2020). Aerodynamic Modeling and Transient Performance Improvement of a Free Jet Altitude Test Facility. Communications in computer and information science.DOI
Chi Ma, Limin Gao, Ruiyu Li, Yu Hou Wu, Heng Jiang (2019). Uncertainty Analysis of Aerodynamic Performance for Tip Clearance Size of Compressor. Proceedings.DOI
Tianyu Gao, Limin Gao, Guanhua Yang, Tianlong Zheng, Ning Ge (2019). Pre-positioning of Optical Components for Pressure Sensitive Paint Measurement Using Prior Ray-tracing Method. Proceedings.DOI
Limin Gao, Chi Ma, Yutong Cai (2019). A Robust Blade Design Method based on Non-Intrusive Polynomial Chaos Considering Profile Error. Journal of Thermal Science.DOI
Bin Zhang, Limin Gao (2019). Topology optimization of convective heat transfer problems for non-Newtonian fluids. Structural and Multidisciplinary Optimization.DOI
Rui-Yu Li, Li-Min Gao, Lei Zhao, Chi Ma, Shiyan Lin (2019). Dominating Unsteadiness Flow Structures in Corner Separation Under High Mach Number. AIAA Journal.DOI
Ruiyu Li, Limin Gao, Shuai Zhang, Yongzeng Li, Tianyu GAO (2018). Application of shear-sensitive liquid crystal coating to visualization of transition and reattachment in compressor cascade. Chinese Journal of Aeronautics.DOI
Ruiyu Li, Limin Gao, Tianlong ZHENG, Guanhua Yang (2018). Experimental investigation on static/dynamic characteristics of a fast-response pressure sensitive paint. Chinese Journal of Aeronautics.DOI
Chi Ma, Limin Gao, Yutong Cai, Ruiyu Li (2017). Robust Optimization Design of Compressor Blade Considering Machining Error.DOI
Shuai Zhang, Li-Min Gao, Tian-Long Zheng, Wei-Min Deng (2017). Numerical Investigations on Characteristic of Fan Based on Two-Way Fluid-Structure Interaction Approach.
高丽敏，李永增，刘晓东，张帅（2016）. 低速轴流压气机叶尖非定常流动试验. 《航空学报》.
Limin Gao, Xiaoquan Hu, Linchuan Tian, Ruiyu Li (2016). Pressure Field Measurement on Compressor Cascade Using Pressure-Sensitive Paint.DOI
Limin Gao (2016). Influence of Blade-root Fillet on Transonic Rotor Performance. Journal of Mechanical Engineering.DOI
Limin Gao, Ruiyu Li, Miao Fang, Yutong Cai (2014). Unsteady Investigation on Tip Flow Field and Rotating Stall in Counter-Rotating Axial Compressor. Journal of Engineering for Gas Turbines and Power.DOI
Limin Gao, Xiaoming Deng, Xudong Feng, Zeyu Yang (2014). Effect of inlet conditions on compressor intermediate duct. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering.DOI
Li-Min Gao (2014). Intensity-based Fast Response PSP Technique and Its Applications.
Li-Min Gao (2014). Effect of Rotor/rotor Interactions on Blades Unsteady Loading.
Limin Gao, Jie Gao, Huan Wang, Qiang Zhou, Bo Liu (2011). PSP experiment of global surface pressure distribution on suction surface of compressor cascade with large curved angle. Journal of Aerospace Power.
Limin Gao, Xudong Feng, Jian Xie (2011). Predication of 3-D Viscous Flowfield of a Centrifugal Impeller. Energy and Power Engineering.DOI
Li-Min Gao (2011). Application of Deterministic Stresses Model in Simulation of Centrifugal Compressor Stage Flow Field.DOI
Qiang Zhou, Bo Liu, Li-Min Gao, Liusheng Chen, M. Shi (2009). Pressure Measurement on Suction Surface of a Single Vane Using Pressure-sensitive Paint.DOI
Limin Gao (2008). Numerical investigation for effect of non-axisymmetric endwall profiling on secondary flow in turbine cascade. Journal of Propulsion Technology.
Li-Min Gao (2008). General Integral Conservation Form of Navier-Stokes Equations and Numerical Application.
Limin Gao, Guang Xi, B Liu, Shaoru Wang (2007). Reduced passage-averaged N-S equations of the threedimensional flowfield in a multi-stage environment. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering.DOI