Zi-Liang Li, Li-Tao Li, Z. Qu, Qingkuo Li, Yanhui Wu (2026). Influence of diffuser integration on aerodynamic performance of a high-load axial compressor used for aero-engine. Chinese Journal of Aeronautics.DOI
Xiang Zhang, Bo Wang, Yanhui Wu, Dong Wang, Chongshan Liu (2026). Suppression of tip leakage vortex breakdown: Aerodynamic mechanism interpretation and POD-assisted knowledge extraction for axisymmetric endwall profiling. Aerospace Science and Technology.DOI
Litao Li, Li Z, Yanhui Wu, Haoguang Zhang, Wuli Chu (2026). Effect of Different Incoming Flow Conditions on the Performance of Axial Flow Diffusers Used for the Jet Engine. Journal of Thermal Science.DOI
Xiang Zhang, Yanhui Wu, Z K Zhang, Dong Wang, Chongshan Liu (2026). Vortex breakdown suppression in a compressor cascade using an l-shaped groove via flow deflection. Aerospace Science and Technology.DOI
Xuyang Shi, Yanhui Wu, Zi-Liang Li (2025). Numerical Investigation of Circumferential Groove Impact on the Secondary Flow Loss Mitigation of Guide Vane in a Variable-Geometry Turbine. Aerospace Science and Technology.DOI
Zi-Liang Li, Zixu Wang, Yanhui Wu (2025). Investigation of upstream wake effect on the endwall flow of a highly loaded compressor cascade at low Reynolds number. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering.DOI
Xuyang Shi, Yanhui Wu, Zi-Liang Li (2025). Numerical study on the effect of design parameters of circumferential multiple grooves on tip leakage flow reduction in a transonic turbine. The Physics of Fluids.DOI
Yanhui Wu, Xiang Zhang, Fan Yang, Stephen Spence (2025). Review of unsteady aerodynamic problems and control strategies for the blade tip flow of axial compressors. Progress in Aerospace Sciences.DOI
Xiang Zhang, Yanhui Wu, Yuanqing Jia, Min Zhang, Chongshan Liu (2025). Research progress on intelligent control technology for aerodynamic stability of axial compressors based on stall warning. Defence Technology.DOI
Ziyun Zhang, Yanhui Wu, Dong Wang, Bo Wang, Lingju HUANG (2025). Experimental and numerical investigation of passive flow control using L-shaped endwall groove in an axial flow compressor stage. Chinese Journal of Aeronautics.DOI
Fan Yang, Yanhui Wu, Stephen Spence, Bo Li, Zhiyang Chen (2024). The investigation on vortex breakdown prior to stall in a compressor rotor with non-uniform tip clearance. The Physics of Fluids.DOI
Zhiyang Chen, Hai-Fei Xiang, Feng Lin, Yanhui Wu, Fan Yang (2024). Numerical investigation into rotating instability and the vortex structure near the tip in a transonic compressor rotor. The Physics of Fluids.DOI
Ziyun Zhang, Yanhui Wu, Zhengtao Guo, Jiezhong Dong (2024). Extraction of geometric features and analysis of flow mechanism of high loaded compressor airfoils at low Reynolds number. The Physics of Fluids.DOI
Xuyang Shi, Yanhui Wu, Haohua Li, Zi-Liang Li (2024). Numerical study on effect of design parameters of the single-circumferential groove on tip leakage flow reduction in a transonic turbine. The Physics of Fluids.DOI
Yapeng Xue, Yanhui Wu, Zi-Liang Li, Ziyun Zhang, Xuyang Shi (2024). Flow mechanism of a highly loaded low pressure turbine cascade with integrated-optimized end wall contouring and root lean. The Physics of Fluids.DOI
Fan Yang, Yanhui Wu (2023). Experimental study on time-frequency characteristics of rotating instability in an isolated axial compressor rotor with variable clearance. Proceedings of Global Power & Propulsion Society.DOI
Yapeng Xue, Zi-Liang Li, Yanhui Wu (2023). Loss Reduction in an Ultra-High-Loaded Low Pressure Turbine Cascade by a Combined Flow Control Strategy. Volume 13B: Turbomachinery — Axial Flow Turbine Aerodynamics.DOI
Fan Yang, Yanhui Wu, Zhiyang Chen, Stephen Spence, Bo Li (2023). The unsteadiness of tip leakage vortex breakdown and its role in rotating instability. The Physics of Fluids.DOI
Ziliang Li, Yanhui Wu, Xingen Lu (2022). Performance Improvement of a Highly Loaded Transonic Centrifugal Compressor with Tandem Impeller and Freeform Blade Configuration. Energies.DOI
Yue Yan, Jianqin Suo, Yanhui Wu (2022). Parameter Optimization of Combustor Dump Diffuser Based on RSM.DOI
Ziyun Zhang, Yanhui Wu, Ziliang Li (2022). Study on Unsteady Flow Characteristic in a Transonic Axial Compressor Rotor at Near Stall Condition.DOI
Ziliang Li, Yapeng Xue, Luwen Feng, Yanhui Wu, Xingen Lu (2022). Impact of the inducer meridional length on the tandem impeller performance within a transonic centrifugal compressor. Proceedings of the Institution of Mechanical Engineers Part A Journal of Power and Energy.DOI
Luwen Feng, Ziliang Li, Yapeng Xue, Yanhui Wu (2022). Investigation of a Highly Loaded Transonic Centrifugal Compressor Using an Advanced Design Method. Proceedings.DOI
周小兵，吴艳辉，薛亚鹏，刘卓奇（2021）. 不同轮缘密封结构封严特性研究. 《工程热物理学报》.
王博，吴艳辉（2020）. 扩压叶栅叶尖非定常流动的涡动力学机理. 《航空学报》.
Zhiyang Chen, Yanhui Wu, Yanwen Zhang, Junwen Gan, Jinhuaiyuan An (2019). Circumferential Propagation Characteristic of Unsteady Flow in a Subsonic Axial Flow Compressor Rotor at Different Reynolds Numbers.DOI
Bo Wang, Yanhui Wu, Kai Liu (2018). Numerical Investigation of Passive Flow Control Using Wavy Blades in a Highly-Loaded Compressor Cascade.DOI
Haoguang Zhang, Xudong Zhang, Yanhui Wu, Wuli Chu, Haiyang Kuang (2018). Flow mechanism of affecting an axial flow compressor performance and stability with cross-blade slot casing treatments. Proceedings of the Institution of Mechanical Engineers Part A Journal of Power and Energy.DOI
Haoguang Zhang, Kang An, Feng Tan, Yanhui Wu, Wuli Chu (2017). Numerical Investigation of Effect of Inlet Distortion on Compressor Flow Field and Stability.DOI
Guangyao An, Yanhui Wu, Jinhua Lang, Zhiyang Chen, Bo Wang, Guowei Yang (2017). Numerical Investigation Into the Mechanism of Tip Flow Unsteadiness in a Transonic Compressor.DOI
Zhiyang Chen, Yanhui Wu, Guowei Yang, Guangyao An, Bo Wang (2017). Investigation Into Flow Mechanism Leading to the Step Change in Aerodynamic Modes of Rotating Instabilities in a Subsonic Axial Compressor Rotor.DOI
Haoguang Zhang, Feng Tan, Kang An, Yanhui Wu, Wuli Chu (2017). Numerical Investigation of Stall Mechanism of an Axial Compressor at Three Different Rotating Speeds.DOI
Wei Wang, Wuli Chu, Haoguang Zhang, Yanhui Wu (2016). Experimental study of self-recirculating casing treatment in a subsonic axial flow compressor. Proceedings of the Institution of Mechanical Engineers Part A Journal of Power and Energy.DOI
Xiangjun Li, Wuli Chu, Yanhui Wu, Haoguang Zhang, Stephen W. T. Spence (2016). Effective end wall profiling rules for a highly loaded compressor cascade. Proceedings of the Institution of Mechanical Engineers Part A Journal of Power and Energy.DOI
Wei Wang, Wuli Chu, Haoguang Zhang, Yanhui Wu (2014). Numerical Investigation on the Effects of Circumferential Coverage of Injection in a Transonic Compressor With Discrete Tip Injection.DOI
Xiangjun Li, Wuli Chu, Yanhui Wu (2014). Numerical investigation of inlet boundary layer skew in axial-flow compressor cascade and the corresponding non-axisymmetric end wall profiling. Proceedings of the Institution of Mechanical Engineers Part A Journal of Power and Energy.DOI
Yanhui Wu, Junfeng Wu, Haoguang Zhang, Wuli Chu (2013). Experimental and Numerical Investigation of Near-Tip Flow Field in an Axial Flow Compressor Rotor: Part II — Flow Characteristics at Stall Inception Condition.DOI
Yanhui Wu, Junfeng Wu, Haoguang Zhang, Wuli Chu (2013). Experimental and Numerical Investigation of Near-Tip Flow Field in an Axial Flow Compressor Rotor: Part I — Flow Characteristics at Stable Operating Conditions.DOI
Xingen Lu, Wuli Chu, Junqiang Zhu, Yanhui Wu (2006). Mechanism of the Interaction Between Casing Treatment and Tip Leakage Flow in a Subsonic Axial Compressor.DOI
吴艳辉，楚武利，卢新根（2005）. 导叶厚度变化对压气机级的性能影响. 《推进技术》.
吴艳辉，楚武利，刘志伟（2005）. 轴流压气机转子性能及间隙流动研究. 《西北工业大学学报》.
Junqiang Zhu, Yanhui Wu, Wuli Chu (2005). Axial Location of Casing Treatment in Multistage Axial Flow Compressors.DOI