徐全勇    副研究员

地址： 北京市海淀区清华大学学研大厦A408室

邮件： xuquanyong@tsinghua.edu.cn

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

航空发动机数字化、智能化研发技术

航空发动机气动热力学

压气机气动布局设计理论

航空发动机气动稳定性预测

研究概况

本人研究专注于航空发动机气动热力学和数智化转型理论与技术，包括：（1）多物理场耦合的数智化设计方法；（2）气动稳定性预测；（3）高负荷压气机气动布局设计理论。

本人的学术研究一直从国家需求出发，用气动热力学和数字化智能化方法探索航空发动机内部复杂流动机理。承担自然科学基金、两机专项、稳定支持、自主科研项目等10项，发表论文38篇，其中SCI论文25篇，EI论文19篇。申请发明专利31项，其中已授权19项。近年来，获得中国产学研合作促进会创新奖、日内瓦发明展2024银奖等奖励，其中数字发动机、虚拟试验等研究成果应用于我国下一代航空发动机研制中。

学术成果

代表性论文列表如下：

[1] Ma Y, Du Z, Xu Q, et al. Flow field reconstruction of compressor blade cascade based on deep learning methods[J]. Aerospace Science and Technology, 2024, 155: 109637.

[2] Liu K, Xu Q, Zhu J. A Multistage Nonlinear Method for Aeroengine Health Parameter Estimation Based on Adjacent Operating Points[J]. Journal of Engineering for Gas Turbines and Power, 2024, 146(10): 101004.

[3] Wu J, Xu Q, Wu F, et al. The icing characteristic of stage 35 compressor blades and its impact on aerodynamic performance[J]. Aerospace Science and Technology, 2024, 150: 109222.

[4] Cheng H, Shahid H, Zhou S, et al. Aerothermal optimization of turbine cascade squealer tip with non-uniform squealer height[J]. Physics of Fluids, 2023, 35(11).

[5] Chen Y, Yang G, Wang L, et al. A Fast Algorithm for Onboard Atmospheric Powered Descent Guidance[J]. IEEE Transactions on Aerospace and Electronic Systems, 2023, 59(5): 6112-6123.

[6] Wu J, Xu Q, Wu F, et al. Droplet Collection Efficiency Regularity of NACA0012 Airfoil Based on the Eulerian Method[J]. Aerospace, 2023, 10(5): 412.

[7] Wang J, Wu F, Xu Q, et al. Local Inverse Mapping Implicit Hole-Cutting Method for Structured Cartesian Overset Grid Assembly[J]. Entropy, 2023, 25(3): 432.

[8] Xu Q, Ren H, Gu H, et al. Large-scale simulation of full three-dimensional flow and combustion of an aero-turbofan engine on sunway taihulight supercomputer[J]. Entropy, 2023, 25(3): 436.

[9] Du Z, Ma Y, Xu Q, et al. Sand discharge simulation and flow path optimization of a particle separator[J]. Entropy, 2023, 25(1): 147.

[10] Xu Q, Wu J, Wu L, et al. Pressure and velocity fluctuations characteristics of the tip clearance flow in an axial compressor stage at the near-stall condition[J]. Aerospace Science and Technology, 2022, 129: 107796.

[11] Zhao Y, Cheng Y, Xu Q, et al. Uncertainty modeling and evaluation of profile measurement by structured light scanner[J]. Measurement Science and Technology, 2022, 33(9): 095018.

[12] Wu J, Xu Q, Zhang Z, et al. Aeroelastic characteristics of inflatable reentry vehicle in transonic and supersonic regions[J]. Computers & Fluids, 2022, 237: 105338.

[13] Zhu H, Wu F, Xu Q, et al. Direct numerical simulation of turbine cascade flow with heat transfer[J]. International Journal of Turbo & Jet-Engines, 2019, 36(4): 445-456.

[14] Zhang R, Xu Q, Fan W. Effect of swirl field on the fuel concentration distribution and combustion characteristics in gas turbine combustor with cavity[J]. Energy, 2018, 162: 83-98.

[15] Xie Z F, Xu Q Y, Guan N X, et al. A new closed-form method for inertia force and moment calculation in reciprocating piston engine design[J]. Science China Technological Sciences, 2018, 61: 879-885.

[16] Chen Z, Zhou M, Xu Q, et al. A novel quasi-3D method for cascade flow considering axial velocity density ratio[J]. International Journal of Turbo & Jet-Engines, 2018, 35(1): 81-94.

[17] Liang F, Li Y, Zhou M, et al. Integrated three-dimensional thermohydrodynamic analysis of turbocharger rotor and semifloating ring bearings[J]. Journal of Engineering for Gas Turbines and Power, 2017, 139(8): 082501.

[18] Liang F, Xu Q, Zhou M. A novel quasi-3D thermodynamic model of oil film bearing with non-Newtonian and temperature-viscosity effects[J]. Industrial Lubrication and Tribology, 2017, 69(5): 638-644.

[19] Liang F, Zhou M, Xu Q. Effects of semi-floating ring bearing outer clearance on the subsynchronous oscillation of turbocharger rotor[J]. Chinese journal of mechanical engineering, 2016, 29(5): 901-910.

[20] Yao Y, Xu Q, Yang Q, et al. Uncertainty evaluation of air flow wall temperature measurement in aero-engine altitude simulation test based on Monte Carlo simulation[C]//9th International Symposium on Test Automation & Instrumentation (ISTAI 2022). IET, 2022, 2022: 383-389.

[21] Liang F, Xu Q, Zhou M. Predicting the Frequency of the Rotor Whirl Excited by Semi-Floating Ring Bearing[C]//International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. American Society of Mechanical Engineers, 2015, 57181: V008T13A074.

[22] Wang J, Wu F, Xu Q, et al. Study on The Method of High Blockage Free-Jet Test in Negative Pressure Condition[C]//33rd AIAA Aerodynamic Measurement Technology and Ground Testing Conference. 2017: 4319.

[23] Liang F, Xu Q, Lan X, et al. The Comparison of Four Pressure-Thermal Models of Oil Film Bearing With the Non-Newtonian and Temperature-Viscosity Effects[C]//International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. American Society of Mechanical Engineers, 2016, 50206: V008T10A022.

[24] Ni Q, Hou A, Tian Y, et al. Design of a Single-Stage Centrifugal Compressor and Numerical Investigation of Simultaneous Adjustment of Inlet Guide Vanes and Diffuser Vanes[C]//ASME International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2013, 56284: V06AT07A041.

[25] Wang Y, Zhou M, Xu Q. The Effect of Intake and Exhaust on the Two-Dimensional Airfoil in a Distributed Propulsion System[C]//ASME International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2016, 50619: V007T09A075.

[26] 胡忠志,曹文宇,何皑,等.数字发动机技术现状、挑战及关键问题[J].航空制造技术,2023,66(21):22-33.

[27] 蒋耀东,徐全勇,马玉林,等.肼基单组元火箭发动机的动态响应[J].航空学报,2023,44(21):348-360.

[28] 吴锋,姚艳玲,王靖元,等.航空发动机内流场数据平均方法研究综述[J].推进技术,2023,44(12):6-20.

[29] 吴锋,刘涛,邓燃,等.可调收敛喷管发动机高空台冲压校准和测量性能近似修正方法[J].航空动力学报,2024,39(10):303-310.

[30] 杜周,马玉林,徐全勇,等.基于ResNet数据驱动的压气机叶型优化[J].航空动力学报,2023,38(07):1592-1603.DOI:10.13224/j.cnki.jasp.20220611.

[31] 杨桥,吴锋,王靖元,等.推力测量中进气冲量的误差分析与不确定度评定[J].航空动力学报,2024,39(10):336-343.

[32] 徐全勇,吴锋.航空发动机整机性能仿真中的功率平衡方法[J].航空动力学报,2022,37(12):2707-2718.DOI:10.13224/j.cnki.jasp.20210194.

[33] 左杨杰,杨艳静,陈伟,等.GH4169合金不同孔形气膜冷却孔疲劳性能对比分析[J].稀有金属材料与工程,2022,51(06):2224-2230.

[34] 杜周,徐全勇,宋振寿,等.基于深度学习的压气机叶型气动特性预测[J].航空动力学报,2023,38(09):2251-2260.

[35] 徐全勇,阙晓斌,吴锋.可控扩散叶型的扩稳优化[J].航空动力学报,2017,32(07):1762-1768.

[36] 陈鹏飞,吴锋,徐全勇,等.可变面积的非对称姿态模拟射流喷管设计与仿真[J].机械工程学报,2018,54(02):184-190.

[37] 徐全勇,侯安平,李绍斌,等.轮毂曲线对跨声速压气机转子性能的影响[J].工程热物理学报,2009,30(05):761-764.

[38] 徐全勇,侯安平,周盛.跨声速轴流压气机转子叶片的掠形优化研究[J].工程热物理学报,2007,(S1):109-112.

专利列表如下：

[1]曹文宇,徐全勇,邵紫鹏,等.方案阶段的结构自动化建模方法和计算机程序产品[P].北京市:CN202410967321.2,2024-08-16.

[2]曹文宇,徐全勇,邵紫鹏,等.发动机的结构自动化转换方法和计算机程序产品[P].北京市:CN202410969147.5,2024-08-16.

[3]徐全勇,吴杰.发动机三维旋转环境下的进气结冰数值模拟方法和装置[P].北京市:CN202410684543.3,2024-08-16.

[4]刘凯,徐全勇,胡忠志.一种具有RVABI结构的航空发动机建模方法[P].北京市:CN202311617986.2,2024-05-31.

[5]徐全勇,吴杰.高空台结冰数据确定方法、装置、电子设备和存储介质[P].北京市:CN202410095695.X,2024-05-24.

[6]徐全勇,吴杰.飞机部件结冰数据确定方法、装置、电子设备和存储介质[P].北京市:CN202410096066.9,2024-04-26.

[7]徐全勇.一种发动机的数据丰富方法、装置及电子设备[P].北京市:CN202211479043.3,2023-04-21.

[8]冷林涛,冯旭栋,吴锋,等.航空发动机高空台建模方法及装置、电子设备和存储介质[P].四川省:CN202211245741.7,2023-01-17.

[9]冯旭栋,吴锋,冷林涛,等.联合仿真装置[P].四川省:CN202211245742.1,2023-01-10.

[10]黄维娜,吴锋,冷林涛,等.航空发动机高空台虚拟试验系统、方法、电子设备及介质[P].四川省:CN202211244140.4,2022-11-11.

[11]徐全勇,王靖元.多孔介质压力损失确定方法、装置、电子设备及存储介质[P].北京市:CN202210418650.2,2022-08-05.

[12]徐全勇,王靖元.多孔介质压力损失确定方法、装置、电子设备及存储介质[P].北京市:CN202210418642.8,2022-08-05.

[13]曹文宇,徐全勇,董学智.可变面积的前涵道引射器和自适应变循环发动机[P].北京市:CN202111402616.8,2022-02-25.

[14]曹文宇,徐全勇,杨俊杰.穿过三层机匣的管路结构[P].北京市:CN202111265452.9,2022-01-21.

[15]曹文宇,谢鹏福,徐全勇.带叶尖风扇的多涵道航空发动机机匣结构[P].北京市:CN202111205513.2,2021-12-03.

[16]徐全勇,王瑞玲.分体式航空发动机性能试验台及试验方法[P].北京市:CN202110321138.1,2021-06-29.

[17]徐全勇,吴锋,冯旭栋,等.涡扇发动机的建模方法[P].北京市:CN201811563778.8,2019-02-22.

[18]谭磊,宋宇,徐全勇,等.电磁驱动机构[P].北京:CN201810619299.7,2018-11-06.

[19]谢之峰,周明,徐全勇,等.平衡机构[P].北京:CN201611100630.1,2017-02-22.

[20]周明,黄旭东,谢芝锋,等.推力矩阵[P].北京:CN201610578642.9,2016-10-12.

[21]谢之峰,周明,徐全勇,等.一种发动机的下缸体总成[P].北京:CN201610344810.8,2016-09-07.

[22]卜建国,周明,吕凯雄,等.用于直升机的混合动力系统及具有其的直升机[P].北京:CN201610116727.5,2016-06-22.

[23]吕凯雄,周明,卜建国,等.分数槽集中绕组记忆电机[P].北京:CN201610012449.9,2016-04-27.

[24]周明,卜建国,吕凯雄,等.无刷电机的双余度控制系统及方法[P].北京:CN201510009415.X,2015-06-24.

[25]卜建国,周明,吕凯雄,等.双凸极永磁记忆飞轮电机[P].北京:CN201510014728.4,2015-04-15.

[26]徐全勇,周明.一种中小型涡轮机湿压缩方法[P].北京:CN201210579788.7,2013-04-24.

[27]徐全勇,黄旭东,周明.一种控制曲率分布的离心叶轮流道设计方法[P].北京:CN201210546397.5,2013-04-03.

[28]徐全勇,黄旭东,周明.一种控制斜率分布的离心叶轮流道设计方法[P].北京:CN201210545524.X,2013-03-27.

[29]周盛,侯安平,阙晓斌,等.航空涡轮风扇发动机压缩系统的紧凑气动布局[P].北京:CN200710119372.6,2007-12-26.