從2008年以來(lái)承擔(dān)本科三年級(jí)《多維氣體動(dòng)力學(xué)基礎(chǔ)》教學(xué)工作，2019年以來(lái)承擔(dān)本科四年級(jí)的《計(jì)算流體力學(xué)》教學(xué)工作。
致力于葉輪機(jī)內(nèi)非定常流動(dòng)機(jī)理研究，發(fā)展高精度數(shù)值模擬方法，探索流體流動(dòng)、葉片振動(dòng)、固體傳熱等相互耦合的機(jī)制和數(shù)值模擬方法，自主開(kāi)發(fā)了針對(duì)航空發(fā)動(dòng)機(jī)的流動(dòng)、傳熱、振動(dòng)的多學(xué)科耦合仿真軟件。目前承擔(dān)了多項(xiàng)重點(diǎn)攻關(guān)課題和預(yù)研項(xiàng)目。近期發(fā)表期刊、會(huì)議論文40余篇，軟件著作權(quán)登記4項(xiàng)，發(fā)明專(zhuān)利5項(xiàng)。
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),
