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一作/通讯作者SCI论文
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.
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.
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.
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.
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.
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.
Ma, J., Yang, G., Zhou, L.*, Ji, L., and Zhang, C. “Effect of a Blade End Slot on Supersonic Compressor Cascade Hub-Corner Separation.” Aerospace Science and Technology, Vol. 118, 2021, p. 107032.
Zhang, C., Ji, L., Zhou, L.*, and Sun, S. “Effect of Blended Blade Tip and Winglet on Aerodynamic and Aeroacoustic Performances of a Diagonal Fan.” Aerospace Science and Technology, Vol. 98, 2020, p. 105688.
Zhang, C., Ji, L., Zhou, L.*, and Zhang, Z. “Effects of Different Blended Blade Tip and Winglets on Aerodynamic and Aeroacoustic Performances of Diagonal Fans.” Aerospace Science and Technology, Vol. 106, 2020, p. 106200.
Li, J., Ji, L., and Zhou, L.* “Design Optimization of a Blended Blade and Endwall in a Compressor Cascade.” Journal of Engineering for Gas Turbines and Power, Vol. 142, No. 2, 2020, pp. 1–11.
Li, X., Ji, L., and Zhou, L. *“Numerical Research on the Trailing-Edge Sweep of Supersonic/Transonic Turbines.” Aerospace Science and Technology, Vol. 99, 2020, p. 105696.
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.
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.
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.
Zhao, R., Zhou, L.*, and Ma, J. “CFD Design of Ventilation System for Large Underground Bus Terminal in Macau Barrier Gate.” Journal of Wind Engineering and Industrial Aerodynamics, Vol. 179, No. May, 2018, pp. 1–13.
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.
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.
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.
一作/通讯作者EI、会议论文
张疏影, 周玲*, 季路成. “通道参数对超声速叶栅性能的影响.” 航空动力学报, Vol. 37, No. 4, 2022, pp. 836–847.
H. L. Zhu, L. Zhou*, J. B. Li, T. T. Meng, L. C. Ji, “Large eddy simulation of corner stall control in a linear compressor cascade by blended blade and end wall method,” Proceedings of Global Power and Propulsion Society , GPPS-TC-2021-188 (2021).
王亮, 周玲*. “基于改进的k-ω-γ转捩模式预测高超声速飞行器气动特性.” 空气动力学报, Vol. 39, No. 3, 2021, pp. 51–61.
马健词, 周玲*, 季路成. “跨声叶栅角区激波/附面层干扰的开槽控制措施.” 航空动力学报, Vol. 36, No. 7, 2021, pp. 1377–1387.
王进, 周玲*, 季路成. “轴流压气机一维特性计算方法简介及展望.” 实验流体力学, Vol. 35, No. 2, 2021.
彭子昂, 于勇, 周玲*, 林博希. HIFiRE-5表面气动热分布的大涡模拟研究. 2022. 第二届中国空气动力学大会
黄明珂, 周玲*, 季路成. 稠度对压气机叶栅通道流动影响的LES研究. 2022. 2022年中国工程热物理学会热机气动热力学和流体机械学术会议
黄明珂, 周玲*, 季路成. 来流附面层厚度对高负荷压气机叶栅通道流动影响的LES研究. 2022. 第五届中国空天推进技术论坛
孙叔贤, 周玲*, 朱熠辰, 蒙童桐, 朱慧玲, 季路成. 高负荷压气机叶栅角区分离流动控制实验研究. 2022. 2022年中国工程热物理学会热机气动热力学和流体机械学术会议
普翔, 周玲*, 季路成. “超跨声速风扇中叶尖间隙影响的两种机制.” 热能动力工程, Vol. 37, No. 4, 2022, pp. 55–63.
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.
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.
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.
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.
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.
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.
非一作/通讯作者SCI论文
Sun, S., Zhou, L., and Ji, L. “Influence of Solidity on Aerodynamic Performance of Axial Supersonic Through-Flow Fan Cascades.” Journal of Propulsion and Power, Vol. 38, No. 4, 2022, pp. 1–14.
Sun, S., Hao, J., Yang, J., Zhou, L., and Ji, L. “Impacts of Tandem Configurations on the Aerodynamic Performance of an Axial Supersonic Through-Flow Fan Cascade.” Journal of Turbomachinery, Vol. 144, No. April, 2022, pp. 1–14.
Li, J., Li, X., Ji, L., Yi, W., and Zhou, L. “Use of Blended Blade and End Wall Method in Compressor Cascades: Definition and Mechanism Comparisons.” Aerospace Science and Technology, Vol. 92, 2019, pp. 738–749.
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.
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.
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.
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.
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.
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.
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