1、受邀担任International Journal of Heat and Mass Transfer、Aerospace and Science Technology、Acta Astronautica、空气动力学报、航空学报等近10个SCI/EI期刊审稿人。
2、受邀担任国家自然科学基金函评专家。
3、受邀做多个学术会议邀请报告并作为分会主席主持学术会议等。
（1）一作/通讯作者SCI论文
[1] H.L. Zhu, L. Zhou*, T. T. Meng, and L. C. Ji, “Corner Stall Control in Linear Compressor Cascade by Blended Blade and Endwall Technique Based on Large Eddy Simulation,” Physics of Fluids, 2021 (accepted).
[2] FU H, ZHOU L*, JI L. The influences of sub boundary layer vortex generator height and attack angle on cross-flows in the hub region of compressors[J]. Chinese Journal of Aeronautics, 2021.
[3] MENG T, YANG G, ZHOU L*等. Full blended blade and endwall design of a compressor cascade[J/OL]. Chinese Journal of Aeronautics, 2021, 34(11): 79–93.
[4] MA J, YANG G, ZHOU L*等. Effect of a blade end slot on supersonic compressor cascade hub-corner separation[J/OL]. Aerospace Science and Technology, 2021, 118: 107032.
[5] LI J, JI L, ZHOU L*. Design Optimization of a Blended Blade and Endwall in a Compressor Cascade[J]. Journal of Engineering for Gas Turbines and Power, 2020, 142(2): 1–11.
[6] ZHANG C, JI L, ZHOU L.*等. Effect of blended blade tip and winglet on aerodynamic and aeroacoustic performances of a diagonal fan[J]. Aerospace Science and Technology, Elsevier Masson SAS, 2020, 98: 105688.
[7] LI X, JI L, ZHOU L*. Numerical research on the trailing-edge sweep of supersonic/transonic turbines[J]. Aerospace Science and Technology, Elsevier Masson SAS, 2020, 99: 105696.
[8] ZHOU L, ZHAO R, YUAN W. Application of Improved k-ω-γ Transition Model to Hypersonic Complex Configurations[J]. AIAA Journal, 2019, 57(5): 2214–2221.
[9] ZHOU L, ZHAO R, MA J. CFD design of ventilation system for large underground bus terminal in Macau Barrier Gate[J]. Journal of Wind Engineering & Industrial Aerodynamics, Elsevier Ltd, 2018, 179(May): 1–13.
[10] ZHOU L, ZHAO R, LI R. A combined criteria-based method for hypersonic three-dimensional boundary layer transition prediction[J]. Aerospace Science and Technology, 2018, 73: 105–117.
[11] ZHOU L, ZHAO R, YUAN W. An investigation of interface conditions inherent in detached-eddy simulation methods[J]. Aerospace Science and Technology, 2018, 74: 46–55.
[12] ZHOU L, ZHAO R, SHI X. An Entropy-Assisted Shielding Function in DDES Formulation for the SST Turbulence Model[J]. Entropy, 2017, 19(3): 93.
[13] ZHOU L, LI R, HAO Z等. Improved k - ω - γ model for crossflow-induced transition prediction in hypersonic flow[J]. International Journal of Heat and Mass Transfer, 2017, 115: 115–130.
[14] ZHOU L, YAN C, HAO Z等. Improved k-ω-γ Model for Hypersonic Boundary Layer Transition Prediction[J]. International Journal of Heat and Mass Transfer, 2016, 94(2016): 380–389.
（2）一作/通讯作者EI、会议论文
[1] H. L. Zhu, L. Zhou, J. B. Li, T. T. Meng, and L. C. Ji, “LARGE EDDY SIMULATION OF CORNER STALL CONTROL IN A LINEAR COMPRESSOR CASCADE BY BLENDED BLADE AND ENDWALL TECHNIQUE,” Proceedings of Global Power and Propulsion Society , GPPS-TC-2021-188 (2021).
[2] 周玲, 阎超, 郝子辉, 孔维萱, 周禹, 转捩模式与转捩准则预测高超声速边界层流动, 航空学报. 37 (2016) 1092–1102. doi:10.7527/S1000-6893.2015.0237.
[3] 周玲, 阎超, 孔维萱, 高超声速飞行器前体边界层强制转捩数值模拟, 航空学报. 35 (2014) 1487–1495. doi:10.7527/S1000-6893.2013.0480.
[4] L. Zhou, R. Zhao, R. Li, C. Yan, W. Zheng, Modeling of hypersonic three-dimensional boundary layer transition using a criteria-based method, in: 21st AIAA International Space Planes and Hypersonics Technologies Conference, 2017. doi:10.2514/6.2017-2192.
[5] 周玲, 黄礼, 孔维萱, 郝子辉, 阎超, 高超声速边界层转捩准则预测方法研究综述, 高超声速技术国际动态. 4 (2016) 32–46.
[6] L. Zhou, C. Yan, Z. Hao, W. Kong, A “laminar + transition criteria” model for hypersonic three-dimensional boundary layer transition prediction, Applied Mechanics and Materials. 798 (2015) 627–631. doi:10.4028/www.scientific.net/AMM.798.627.
[7] 周玲, 阎超, 郝子辉, 两种工程转捩预测方法对高超声速横流转捩的预测性能研究, 中国力学大会, 2015.
（3）非一作/通讯作者SCI论文
[1] ZHAO R, WEN C Y, LONG T H,TIAN X D, ZHOU L. Spatial Direct Numerical Simulation of the Hypersonic Boundary-Layer Stabilization Using Porous Coatings[J]. AIAA Journal, 2019, 57(11): 5061–5065.
[2] LI J, LI X, JI L,YI W L, ZHOU L. Use of Blended Blade and End Wall method in compressor cascades: Definition and mechanism comparisons[J]. Aerospace Science and Technology, Elsevier Masson SAS, 2019, 92: 738–749.
[3] HAO Z, YAN C, ZHOU L等. Development of A Boundary Layer Parameters Identification Method for Transition Prediction with Complex Grids[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2017, 231(11): 2068–2084.
[4] QIN Y, YAN C, HAO Z, ZHOU L. A Laminar Kinetic Energy Transition Model Appropriate for Hypersonic Flow Heat Transfer[J]. International Journal of Heat and Mass Transfer, Elsevier Ltd, 2017, 107: 1054–1064.
[5] HAO Z, YAN C, QIN Y, ZHOU L. Improved γ-Reθt Model for Heat Transfer Prediction of Hypersonic Boundary Layer Transition[J]. International Journal of Heat and Mass Transfer, Elsevier Ltd, 2017, 107: 329–338.
[6] DU R, YAN C, QU F, ZHOU L. Investigation of all-speed schemes for turbulent simulations with low-speed features[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2017, 0(37): 095441001668714.
（4）非一作/通讯作者EI、会议论文
[1] HAO Z, YAN C, QIN Y, ZHOU L. Study of Hypersonic Boundary Layer Transition with Different Reynolds Numbers[C]//2016 7th International Conference on Mechanical and Aerospace Engineering (ICMAE). IEEE, 2016: 582–586.
[2] 郝子辉, 阎超, 周玲. k-ω-γ模式对转捩影响因素的预测性能研究[J]. 力学学报, 2015, 47(2): 215–222.
近年来出版专著
赵瑞，周玲，阎超，季路成，《湍流与转捩数值模拟方法》，ISBN：9787564076269，2019.3
项目承担情况
1、主持“两机”重大专项子课题1项
2、主持国家自然科学基金青年科学基金1项
3、主持国家自然科学基金面上项目1项
4、主持中国航空发动机研究院气动仿真软件项目2项
5、主持中国航发沈阳发动机研究所高负荷静叶端区流动控制项目1项
6、参与国家“航空发动机及燃气轮机”两机专项项目子课题2项
7、参与航天一院、三院以及航天五院转捩预测项目3项
（课题组学生科研任务源于课题组获得的国家长期的纵向资助项目，以帮助学生在一个科研方向上的持续、深入研究。）
教学工作
指导硕士研究生9名，协助指导博士研究生10名。
主要讲授课程：1、本科生《内流空气动力学》，2、留学生课程《Aerodynamics》，3、研究生《高等计算流体力学》
