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个人简介

教育背景 2000.09~2004.07,北京航空航天大学,飞行器动力工程专业,本科,学士 2004.09~2006.07,北京航空航天大学,航空宇航推进理论与工程专业,硕士,师从周盛教授 2006.09~2010.01,北京航空航天大学,航空宇航推进理论与工程专业,博士,师从周盛教授 工作履历 2010.04~2012.08,北京大学,湍流与复杂系统国家重点实验室,博士后,师从陈十一院士 2012.08~2019.08,清华大学,航天航空学院,助理研究员、副研究员 2019.08~至今, 清华大学,航空发动机研究院,副研究员

研究领域

航空发动机气动热力学与数值仿真方法 航空发动机整机性能匹配与部件融合设计方法研究 航空发动机叶轮机械流动机理与设计技术 航空发动机气动稳定性评估预测 航空发动机流固热多场耦合研究 分布式新概念动力系统

近期论文

查看导师新发文章 (温馨提示:请注意重名现象,建议点开原文通过作者单位确认)

Rongchun Zhang, Quanyong Xu, Weijun Fan, Effect of swirl field on the fuel concentration distribution and combustion characteristics in gas turbine combustor with cavity, Energy, Volume 162, 2018, Pages 83-98. Xie Zhifeng, Xu Quanyong, Guan Nanxiang, et al, A new closed-form method for the inertia force and moment calculation in reciprocating piston engine design, Science China Technological Sciences, June 2018, Volume 61, Issue 6, pp 879–88. Haitao Zhu, Feng Wu, Quanyong Xu, et al, Direct Numerical Simulation of Turbine Cascade Flow with Heat Transfer, International Journal of Turbo & Jet-Engine, 2017. Zhiqiang Chen, Ming Zhou, Quanyong Xu, A Novel Quasi-3D Method for Cascade Flow Considering Axial Velocity Density Ratio, International Journal of Turbo and Jet-Engines. June 2016. Liang Feng, Zhou Ming, Xu Quanyong, Effects Of Semi-Floating Ring Bearing Outer Clearance On The Subsynchronous Oscillation Of Turbocharger Rotor, Chinese Journal Of Mechanical Engineering, 2016. Liang, Feng, Xu Quanyong, Zhou, Ming, A Novel Quasi-3D Thermodynamic Model Of Oil Film Bearing With Non- Newtonian and Temperature- Viscosity Effects, Industrial Lubrication And Tribology, accepted, published in 2017. Quanyong Xu, Yantao Yang, Reynolds-Stress-Constrained Large Eddy Simulation Of Separation Flows In A U-Duct, Propulsion And Power Research, Volume 3, Issue 2, June 2014, Pages 49–58. Feng Wu, Quanyong Xu,Qiannan Xu,et al, Distortion flow field research on flat baffle experiment in round duct, ASME Turbo Expo 2018, GT2018-76328. Juanjuan Wang, Feng Wu, Xu Quanyong, Study on the method of high blockage free-jet test in negative pressure condition,33rd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, AIAA 2017-4319. Yongsheng Wang, Zhou Ming, Xu Quanyong, The effect of intake and exhaust on the two dimensional airfoil in a distributed propulsion system, ASME, IMECE Proceedings, 2016. Feng Liang, Quanyong Xu, Ming Zhou, Predicting The Frequency Of The Rotor Whirl Excited By Semi-Floating Ring Bearing, ASME 2015 IDET. Ni Qi, Hou, A., Tian, Y., Xu Quanyong, Design Of a Single-Stage Centrifugal Compressor and Numerical Investigation of Simultaneous Adjustment of Inlet Guide Vanes And Diffuser Vanes, ASME, IMECE Proceedings, 2013. 徐全勇,阙晓斌,吴锋, 可控扩散叶型的扩稳优化研究,航空动力学报,2017 Vol. 32, No. 7.

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