李健
助理研究员
3044AM永利集团A438
lijian0320@sjtu.edu.cn
+86 13111114268
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2019年-2023年，上海交通大学，博士
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2021年-2022年，Politecnico di Torino，Co-operative student
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2016年-2019年，哈尔滨工程大学，硕士
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2012年-2016年，哈尔滨工程大学，学士
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2025年-至今，上海交通大学，助理研究员
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2023年-2025年，上海交通大学，博士后
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2024年-2025年，中国航发商用航空发动机有限责任公司，挂职借调
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叶轮机械气动热力学
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轴流压气机通流计算分析
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复杂非线性系统降阶建模
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国家自然科学基金青年基金
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国家自然科学基金联合基金
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国家自然科学基金面上项目
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Li J, Qiang X, Teng J, et al. Comparison of turbulence models for tip leakage flow of a large clearance compressor cascade with casing motion[J]. Aerospace Science and Technology, 2025: 110545.
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Qiang X, Lu Y, Li J. Bleed air CFD modelling in aerodynamic simulation of A heavy duty gas turbine compressor[J]. Energy, 2024, 299: 131423.
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Qiang X, Li J, Ma Y. Experimental test of a compressor cascade with non-axisymmetric end-wall contouring at off-design conditions[J]. Applied Thermal Engineering, 2024, 240: 122208.
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Li J, Teng J, Ferlauto M, et al. An improved stall prediction model for axial compressor stage based on diffuser analogy[J]. Aerospace Science and Technology, 2022, 127: 107692.
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Li J, Teng J, Zhu M, et al. Loss prediction of axial compressors using genetic algorithm–back propagation neural network in throughflow method[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2022, 236(8): 1577-1589.
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Li J, Teng J, Zhu M, et al. A viscous blade body force model for computational fluid dynamics–based throughflow analysis of axial compressors[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2021, 235(16): 2493-2503.
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Li J, Qiang X. The Aerodynamic Interaction of Seal Leakage and Mainstream Flows in a Compressor Cascade With Non-Axisymmetric Endwall[C]//Turbo Expo: Power for Land, Sea, and Air. American Society of Mechanical Engineers, 2024, 88056: V12AT29A009.
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Li J, Wu D, Teng J, et al. The effects of incidence and deviation on the CFD-based throughflow analysis[C]//Turbo Expo: Power for Land, Sea, and Air. American Society of Mechanical Engineers, 2020, 84065: V02AT32A010.
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