发表研究论文70余篇，其中发表在AIAA Journal、Physics of Fluids等行业顶级/重要期刊SCI论文42篇，部分一作/通讯作者SCI论文罗列如下。
[1] Zhu, H., Zhou, L.*, Li, J., Sun, S., and Ji, L., “An Improved Criterion for Predicting Corner Stall in Axial Compressors with Varying Dihedral Angles,” Chinese Journal of Aeronautics, 2025, p. 103726.
[2] Zhou, L., Suo, Y., Khoo, B. C., Zhu, H., and Ji, L., “Large Eddy Simulation of Inflow Velocity Effects on Flow Characteristics in a Square-Section Diffuser,” Physics of Fluids, Vol. 37, No. 8, 2025, p. 085102.
[3] Meng, Q., Lei, J., Wu, S., Yuan, C., Yu, J., and Zhou, L.*, “High Reynolds and Mach Number Effects on Transition Behavior on a Flared Cone–Swept Fin Configuration,” Physics of Fluids, Vol. 37, No. 6, 2025, p. 064106.
[4] Li, X., Meng, T., Zhou, L.*, Li, W., and Ji, L., “Optimization and Numerical Investigation of Combined Design of Blade and Endwall on Rotor 67,” International Journal of Turbo & Jet-Engines, Vol. 41, No. 2, 2024, pp. 267–277.
[5] Fu, H., Zhou, L.*, and Ji, L. “Influence of Sub Boundary Layer Vortex Generator Height and Attack Angle on Cross-Flows in the Hub Region of Compressors.” Chinese Journal of Aeronautics, Vol. 35, No. 8, 2022, pp. 30–44.
[6] Meng, T., Li, X., Zhou, L.*, Zhu, H., Li, J., and Ji, L. “Large Eddy Simulation and Combined Control of Corner Separation in a Compressor Cascade.” Physics of Fluids, Vol. 34, No. 7, 2022, p. 075113.
[7] Zhu, H., Zhou, L.*, Fu, H., Sun, S., Ji, L., and Lin, B. “Investigation on Corner Stall Prediction and Flow Control by Blended Blade and End Wall Technology in a Compressor Cascade Based on Modified Spalart-Allmaras Model.” Physics of Fluids, Vol. 34, No. 11, 2022, p. 115147.
[8] Zhang, S., Zhou, L.*, and Ji, L. “Investigation of Hysteresis Loop in the Starting Process of Supersonic Cascade.” AIAA Journal, Vol. 60, No. 4, 2022, pp. 2685–2693.
[9] Meng, T., Yang, G., Zhou, L.*, and Ji, L. “Full Blended Blade and Endwall Design of a Compressor Cascade.” Chinese Journal of Aeronautics, Vol. 34, No. 11, 2021, pp. 79–93.
[10] Zhu, H., Zhou, L.*, Meng, T., and Ji, L. “Corner Stall Control in Linear Compressor Cascade by Blended Blade and Endwall Technique Based on Large Eddy Simulation.” Physics of Fluids, Vol. 33, No. 11, 2021, p. 115124.
[11] Zhou, L., Zhao, R., and Yuan, W. “Application of Improved K-ω-γ Transition Model to Hypersonic Complex Configurations.” AIAA Journal, Vol. 57, No. 5, 2019, pp. 2214–2221.
[12] Zhou, L., Zhao, R., and Li, R. “A Combined Criteria-Based Method for Hypersonic Three-Dimensional Boundary Layer Transition Prediction.” Aerospace Science and Technology, Vol. 73, No. 5, 2018, pp. 105–117.
[13] Zhou, L., Zhao, R., and Yuan, W. “An Investigation of Interface Conditions Inherent in Detached-Eddy Simulation Methods.” Aerospace Science and Technology, Vol. 74, 2018, pp. 46–55.
[14] Zhou, L., Zhao, R., and Shi, X.-P. “An Entropy-Assisted Shielding Function in DDES Formulation for the SST Turbulence Model.” Entropy, Vol. 19, No. 3, 2017, p. 93.
[15] Zhou, L., Li, R., Hao, Z., Zaripov, D. I., and Yan, C. “Improved K-ω-γ Model for Crossflow-Induced Transition Prediction in Hypersonic Flow.” International Journal of Heat and Mass Transfer, Vol. 115, 2017, pp. 115–130.
[16] Zhou, L., Yan, C., Hao, Z. H., and Du, R. F. “Improved k – ω – γ Model for Hypersonic Boundary Layer Transition Prediction.” International Journal of Heat and Mass Transfer, Vol. 94, No. 2016, 2016, pp. 380–389.
其他学术成果
（1）教材
[1] 《湍流与转捩数值模拟方法》，赵瑞，周玲，阎超，季路成，2019.3
（2）申请/授权发明专利30余项，获批软件著作权6项
主持/参与科研项目
1、 主持国家自然科学基金等国家级纵向项目4项，参与国家级纵向项目4项
2、 主持横向项目17项，与中国航空发动机研究院、中国科学院工程热物理研究所等行业内近10家重要科研单位均有合作
教学工作
本科生课程：《内流空气动力学》、《Aerodynamics》（留学生课程）、《流体力学核心贯通课II》
研究生课程：《高等计算流体力学》
