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周创鑫，男，1996年生，工学博士，讲师。长期从事航空发动机气动热力学研究。负责全国重点实验室开放基金一项，参与包括国家自然科学基金重点项目、LJ专项、MJ专项在内的多项重大科研项目，依托项目发表十余篇SCI索引论文，入选2024年度中国航空学会博士学位论文托举工程（共15人）。

部分论文列表：

[1] Zhou C, Li Z, Huang S, et al. Numerical Investigation on the Aerodynamic Performance and Flow Mechanism of a Fan with a Partial-Height Booster Rotor[J].

     Aerospace Science and Technology, 2020, 109(4): 106411.

[2] Zhou C, Zhao S, Lu X. Investigating the Aerodynamic Design of a Novel Tandem Fan with a Partial-Span Booster Rotor[J]. Aerospace Science and Technology,

     2022, 132(12): 108018.

[3] Zhou C, Zhao S, Lu X. Flow Mechanism of a New Concept Transonic Tandem Fan Stage under the Design and Off-Design Conditions[J]. Aerospace, 2022,

     9(11): 686.

[4] Zhou C, Zhao S, Yang C, et al. The Matching Characteristics and Flow Mechanisms of Partial-Height Booster Rotor and Fan Rotor for a High-Throughflow

     Fan[J]. Proceedings of the Institution of Mechanic Engineers, Part C: Journal of Mechanical Engineering Science, 2022, 236(23): 11240-11255.

[5] Zhou C, Zhao S, Lu X. Investigations on the Unsteady Flow Mechanism of the High-Throughflow Fan with Partial-Height Booster Rotor[J]. Proceedings of the

     Institution of Mechanic Engineers, Part A: Journal of Power and Energy, 2023, 237(5): 939-952.

[6] Zhou C, Zhao S, Yang C, et al. The Mechanism of Axial Arrangement Affecting the Performance for Tandem Rotor with Partial-Height Booster Rotor in

     High-Throughflow Fan[R]. GPPS Paper, TC-0123, 2021.

[7] 周创鑫, 李紫良, 赵胜丰等. 前置部分叶高增压转子风扇气动性能研究[J]. 工程热物理学报, 2021, 42(06): 1413-1422.

[8] 周创鑫, 成金鑫, 黄松等. 基于贝塞尔曲面参数化方法的1.5级高负荷轴流压气机气动优化[J]. 航空动力学报, 2021, 36(04): 673-686.

[9] Cheng H, Zhou C, Lu X, et al. Robust Aerodynamic Optimization and Design Exploration of a Wide-Chord Transonic Fan under Geometric and Operational

     Uncertainties[J]. Energy, 2023: 128011.

[10] Li Z, Han G, Zhou C, et al. Quantitative Analysis on Influence of Secondary Flow for Centrifugal Impeller Internal Flow[J]. Physics of Fluids, 2023, 35: 076113.

[11] Cheng H, Li Z, Zhou C, et al. Effect of Blade Surface Cooling on a Micro Transonic Axial Compressor Performance at Low Reynolds Number[J]. Applied Thermal

       Engineering, 2023: 120353.

[12] Cheng H, Zhou C, Li Z, et al. Uncertainty quantification and sensitivity analysis on the aerodynamic performance of a micro transonic compressor[J]. Aerospace

       Science and Technology, 2023, 141: 108569.

[13] Zhou S, Zhao S, Zhou C, et al. Optimal Design and Analysis of a High-Load Supersonic Compressor Based on a Surrogate Model[J]. Aerospace, 2022,

       9(11): 686.

[14] Cheng H, Wang M, Zhou C, et al. Influence of Surface Roughness on a Highly Loaded Axial Compressor Stage Performance at Low Reynolds Number[J].

       International Journal of Aerospace Engineering, 2021, 2021: 1-18.

[15] Huang S, Zhou C, Yang C, et al. Effect of Backward Sweep on Aerodynamic Performance of a 1.5-Stage Highly Loaded Axial Compressor[R]. ASME Paper,

       GT2020-14262, 2020.

[16] 周仕佶, 周创鑫, 赵胜丰等.基于表面热膜测试的低速风扇附面层流动研究[J]. 推进技术, 2023, 44(05): 264-271.

联系方式：

zhouchuangxin@hotmail.com

[1] 航空发动机内流气动热力学

[2] 高性能叶轮机械设计及优化

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[1]  2018.9- 2023.6

中国科学院工程热物理研究所 | 动力机械及工程 | With Certificate of Graduation for Doctorate Study | Doctoral Degree in Engineering

[2]  2014.9- 2018.6

湖南大学 | 能源与动力工程 | University graduated | Bachelor's Degree in Engineering

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