航空宇航推进理论与工程方向硕士生导师
研究方向：
1.航空发动机/燃气轮机燃烧室内复杂湍流燃烧特性研究
2.新能源/混合燃料的层流燃烧特性实验研究及数值计算
3.航空发动机燃油喷雾两相流及非平衡等离子体助燃技术研究
4.非均匀混合的可燃气体火焰加速与爆轰机理的数值方法研究
个人简介：
郑玮琳，女，2016年6月博士毕业于北京航空航天大学流体力学专业，2016年9月至2017年11月于美国马里兰大学航空航天学院担任博士后研究员，2018年5月至今于沈阳航空航天大学航空发动机学院担任副教授。
科研项目：
主持辽宁省博士启动基金项目、中国科学院光电研究院项目、校博士启动基金项目，参与航空发动机及燃气轮机重大专项基础研究项目、美国ALPHA基金项目、辽宁省自然科学基金项目、以及973计划项目中飞行器气动力学与光学设计中的关键湍流问题的研究。
论文发表:
[1]W.L. Zheng; F. Xie; C. Yan; W. Zeng, A hybrid RANS/LES approach with scale-adaptive capabilities for highly separated flows, International Journal of Computational Fluid Dynamics, 2019， : 1-13. (SCI, IF:1.384)
[2]W.L. Zheng; C.R. Kaplan; R.W. Houim; E.S. Oran, Flame acceleration and transition to detonation: effects of a composition gradient in a mixture of methane and air, Proceedings of the Combustion Institute, 2019, 37(3): 3521-3528. (SCI, IF:3.299)
[3]W.L. Zheng, Yan Chao, Liu Hongkang and Luo Dahai. Comparative assessment of SAS and DES turbulence modeling for massively separated flows. Acta Mechanica Sinica, 2016, 32(1): 12-21. (SCI, IF:1.324)
[4]W.L. Zheng, Wang Yankui, Shan Jixiang, Deng Xueying and Tian Wei. Interference mechanism of engine exhaust on civil aircraft drag performance, Journal of Aircraft, 2012, 49(6): 2001-2006. (SCI, IF 0.835)
[5]W.L. Zheng, Yan Chao. A Scale-adaptive simulation method based on S-A turbulence model. The 6th International Conference on Mechanical and Aerospace Engineering, 2015, Roma, Italy. (Oral presentation)
[6]郑玮琳, 阎超. XY-SAS 模型中不同网格尺度限制器的影响.北京航空航天大学学报, 2014, 40(12):1725-1729. (EI)
[7] J. Liu, E.J. Hu, W. Zeng, W.L. Zheng*, A new surrogate fuel for emulating the physical and chemical properties of RP-3 kerosene, Fuel, 259,2020. (SCI, IF:5.128)
[8]W. Zeng; J. Liu; Y. Liu; H.A. Ma; W.L. Zheng, Reaction kinetic simulation of the combustion and emission characteristics of a dual-fuel aero-engine, Fuel, 2019, 237(1): 352-360. (SCI, IF:5.128)
[9]C.R. Kaplan, W.L. Zheng, H.H. Xiao, and E.S. Oran. Optimization of chemical-diffusive models for deflagration-to-detonation transition calculations. 10th U.S. National Combustion Meeting, 2017, College Park, Maryland.
[10] L. Zhou, R. Zhao, R.F. Li, C. Yan, W.L. Zheng. Modeling of hypersonic three-dimensional boundary layer transition using a criteria-based method. 21st AIAA International Space Planes and Hypersonics Technologies Conference, 2017, Xiamen, China.
[11] X.Y. Wang, C. Yan, W.L. Zheng, K. Zhong, Y.F. Geng. Laminar and turbulent heating predictions for mars entry vehicles. Acta Astronautica, 2016, 128: 217-228. (SCI, IF 1.536)
[12] D.H. Luo, C. Yan, W.L. Zheng, W. Yuan. A new PANS model for unsteady separated flow simulations. Applied Mechanics and Materials, 2015, 721: 182-186. (EI)
[13] 李雯, 崔燚, 王浚, 郑玮琳.月球受光面上月尘静电浮扬特性分析. 北京航空航天大学学报, 2010, 10: 1199-1202. (EI)
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