从2008年以来承担本科三年级《多维气体动力学基础》教学工作，2019年以来承担本科四年级的《计算流体力学》教学工作。
致力于叶轮机内非定常流动机理研究，发展高精度数值模拟方法，探索流体流动、叶片振动、固体传热等相互耦合的机制和数值模拟方法，自主开发了针对航空发动机的流动、传热、振动的多学科耦合仿真软件。目前承担了多项重点攻关课题和预研项目。近期发表期刊、会议论文40余篇，软件著作权登记4项，发明专利5项。
1.Zheng, Y., Jin, X.B., Yang, H. Fast-moving Mesh Method and Its Application to Circumferential Non-uniform Tip Clearance in a Single-stage Turbine, Journal of Applied Fluid Mechanics, 2024, 17(8): 1759–1773, DOI: 10.47176/jafm.17.8.2371
2.Yang, H., Liang, H., Zheng, Y. Effect of Intake Acoustic Reflection on Blade Vibration Characteristics, Aerospace, 2024, 11(5), 358, DOI: 10.3390/aerospace11050358
3.Yun Zheng, Xiubo Jin and Hui Yang, Low-Engine-Order Forced Response Analysis of a Turbine Stage with Damaged Stator Vane, Entropy 2024, 26, 4. DOI: 10.3390/e26010004
4.Zheng, Y.; Gao, Q.; Yang, H. Forced Response Analysis of an Embedded Compressor Rotor Induced by Stator Disturbances and Rotor–Stator Interactions. Aerospace 2023, 10, 398. DOI: 10.3390/aerospace10050398
5.Lei, D.; Yang, H.; Zheng, Y.; Gao, Q.; Jin, X. A Modified Shielding and Rapid Transition DDES Model for Separated Flows. Entropy 2023(25), 613. DOI: 10.3390/e25040613
6.Yun Zheng, Xiubo Jin and Hui Yang，Effects of Asymmetric Vane Pitch on Reducing Low-Engine-Order Forced Response of a Turbine Stage, Aerospace 2022, 9(11), 694. DOI: 10.3390/aerospace911069
7.Yun ZHENG , Qingzhe GAO, Hui YANG, Non-synchronous blade vibration analysis of a transonic fan, Chinese Journal of Aeronautics, 2023, 36(1), pp. 178-190, DOI: 10.1016/j.cja.2022.04.011
8.Yun Zheng, Qingzhe Gao, Hui Yang, Kang Xu, Aeroelastic vibration analysis of a 1.5 stage compressor, Propulsion and Power Research, 2020, 9(1):26-36, DOI: 10.1016/j.jppr.2019.11.001
9.ZHENG Yun, YANG Hui, Coupled Fluid-structure Flutter Analysis of a Transonic Fan, Chinese Journal of Aeronautics, 2011, 24(3), pp. 258-264
10.Zheng Yun, L. HE. Multigrid Upwind Euler/Navier-Stokes Computation on adaptive Unstructured Meshes，Royal Aeronautic Journal，2001.4
11.Wang Peng, Zheng Yun, Zou Zhengping, Qi Lei, Zhou Zhixiang，A novel multi-fidelity coupled simulation method for flow systems, Chinese Journal of Aeronautics, 2013 26(4),pp. 868-875
12.Haiyang Hu, Yihan Li, Ziyu Wei, Yun Zheng, Optimization of the MSMGWB model used for the calculation of infrared remote sensing signals from hot combustion gases of hydrocarbon fuel, Infrared Physics & Technology, 2020(107),
