2013.9 — 2018.12 西北工业大学 航空宇航科学与技术专业，博士 2011.9 — 2014.4 西北工业大学 航空宇航推进理论与工程专业，硕士 2007.9 — 2011.7 西北工业大学 飞行器动力工程专业，学

2018.12 — 至今 大连海事大学 能源与动力工程系，讲师

[1] Xiangjun Li, Stephen Spence and Yanhui Wu, The interaction between inlet guide vanes and the impeller recirculating flow in a centrifugal compressor and the resulting impact on flow range, Proceedings of ASME Turbo Expo 2018, GT2018- 75097. [2] Xiangjun Li, Stephen Spence, The impact of the multiple reference frame interface on modelling the interaction between IGVs and the impeller in turbocharger compressors, Proceedings of ASME Turbo Expo 2017, GT2017- 63499 [3] Xiangjun Li, Stephen Spence, Wuli Chu, Hua Chen, Lee Gibson, Flow Control by Slot Position and Noise Baffle in a Self-Recirculation Casing Treatment on an Axial FanRotor. International Journal of Rotating Machinery, 2017, No.9509212. [4] Wuli Chu, Xiangjun Li, Yanhui Wu, Haoguan Zhang, Reduction of end wall loss in axial compressor by using non-axisymmetric profiled end wall: A new design approach based on end wall velocity modification. Aerospace Since and Technology, 55, 2016. [5] Xiangjun Li, Wuli Chu, Yanhui Wu, Haoguang Zhang, Stephen Spence, Effective end wall profiling rules for a highly loaded compressor cascade. Proc IMechE, Part A: J Power and Energy. 230(6), 2016. [6] Xiangjun Li, Wuli Chu and Yanhui Wu, Numerical investigation of inlet boundary layer skew in axial-flow compressor cascade and the corresponding non-axisymmetric end wall profiling, Proc IMechE, Part A: J Power and Energy, Vol.288(6), 2014. [7] 李相君, 楚武利, 张皓光, 高负荷轴流压气机叶栅二次流动与损失关联性探讨, 推进 技术, 35(7), 2014. [8] 李相君, 楚武利, 张皓光, 高负荷跨声速轴流压气机周向浅槽处理机匣扩稳机理, 推 进技术, 34(5), 2013