教育经历
2006年9月-2011年1月，清华大学，航天航空学院，博士
2004年9月-2006年7月，清华大学，航天航空学院，硕士
2000年9月-2004年7月，清华大学，工程力学系，本科
工作经历
2017年7月 - 至今，清华大学，航天航空学院，特别研究员，副教授
2015年1月 - 2016年1月，美国圣母大学，Meng Wang课题组访问助理教授
2012年12月- 2017年7月，清华大学，航天航空学院，讲师、助理教授
2011年1月 - 2012年12月，清华大学，航天航空学院，博士后
研究方向
飞行器空气动力学
气动优化设计
自然层流技术
非定常流动与气动噪声模拟
飞机结冰空气动力学
人工智能在气动中的应用
学术兼职和荣誉
2021年中组部“万人计划”青年拔尖人才
2017年度航空学会青年科技奖
ICAS (International Council of Aeronautical
Sciences)青年委员
APISAT（亚太航空科学会议）委员
AIAA (American Institute of Aeronautics and
Astronautics) lifetime高级会员
航空学报、CJA青年编委
AIAA J、CJA、AST、Sci. China等期刊审稿人，2017年度航空学报“优秀审稿专家”
力学学会流固耦合专业委员会委员、工业流体力学专业组委员
空气动力学会计算流体力学专委会委员
主要论文
1)M Xiao, Y Zhang, “Improved
Prediction of Flow Around Airfoil Accreted with Horn or Ridge Ice”, AIAA
Journal, 2021, 59 (6), 2318-2327.
2)S Zhang, H Li, Y Zhang, H Chen, “Aerodynamic
Prediction of High-Lift Configuration Using k-(v^ 2)-ω Turbulence
Model”, AIAA Journal, 2021, accepted.
3)S Zhang, R Li, Y Zhang, H Chen, “Aerodynamic
Optimization and Noise Reduction of a Two-Stage Series Compact Fan”, Journal
of Aerospace Engineering, 2021, 34 (5), 04021057.
4)R Li, Y Zhang, H Chen, “Learning
the aerodynamic design of supercritical airfoils through deep reinforcement
learning”, AIAA Journal , 2021, 59 (10), 3988-4001 .
5)R Li, Y Zhang, H Chen, “Pressure
distribution feature-oriented sampling for statistical analysis of
supercritical airfoil aerodynamics”, Chinese Journal of Aeronautics,
online, 2021.
6)Y Yin, P Yang, Y Zhang, H Chen, S
Fu, “Feature selection and processing of turbulence modeling based on an
artificial neural network”, Physics of Fluids, 2020, 32 (10),
105117. (Featured article)
7)Xiao, M., Zhang, Y., “Assessment
of the SST-IDDES with a Shear-layer-adapted Subgrid Length Scale for Attached
and Separated Flows”, International
Journal of Heat and Fluid Flow, 2020, 85, 108653.
8)Zhang Y.,
Yan C., Chen H., “An inverse design method for airfoils based on pressure
gradient distribution”, Energies,
2020, 13 (13), 3400.
9)Xiao, M., Zhang, Y., Zhou, F.,
“Numerical Investigation of the Unsteady Flow past an Iced Multielement
Airfoil”, AIAA Journal, 2020, 58
(9), 3848-3862.
10)Li
H., Zhang Y., Chen H., “Aerodynamic Prediction of Iced Airfoils based on
a Modified Three-Equation Turbulence Model”, AIAA Journal, 2020, 58 (9), 3863-3876.
11)Zhang
Y., Yan C., Chen H., Yin Y., “Study of Riblet Drag
Reduction for an Infinite Span Wing with Different Sweep Angles”, Chinese Journal of Aeronautics, 2020,
33 (12), 3125-3137.
12)Yang
J, Zhang Y, Chen H, Fu S, “Flow separation control in a conical diffuser
with a Karman-vortex generator”, Aerospace
Science and Technology, 2020, 106, 106076.
13)Yang
J, Zhang Y, Chen H, Fu S, “Unsteady flow control of a plane diffuser
based on a Karman vortex generator”, AIP
Advances, 2020, 10 (5), 055314.
14)Niu,
W., Zhang, Y., Chen, H., Zhang, M., “Numerical Study of a Supercritical
Airfoil/Wing with Variable-Camber Technology”, Chinese Journal of Aeronautics, 2020, 33(7), 1850-1866.
15)Yin,
Y., Zhang, Y., “Optimization and Analysis of a Blown Flap Based on a Multielement
Airfoil”, Journal of Aircraft,
2020, 57 (1), 62-75.
16)Li,
H., Zhang, Y., Chen, H., “Optimization of Supercritical Airfoil
Considering the Ice-Accretion Effects”, AIAA
Journal, 2019, 57 (11), 4650-4669.
17)Zhang,
Y., Yin, Y., “Study on Riblet Drag Reduction
Considering the Effect of Sweep Angle”, Energies,
2019, 12:3386.
18)Xiao,
M., Zhang, Y., Zhou, F., “Numerical Study of Iced Airfoils
with Horn Features Using Large-Eddy Simulation”, Journal of Aircraft, 2019, 56(1): 94-107.
19)Song,
W., Zhang, Y., Chen, H, et al. “Transonic Compressor Blade
Optimization Integrated with Circumferential Groove Casing Treatment”, Journal of Turbomachinery, 2019, 141(3)
20)Zhang,
Y., Chen, H., Fu, S., et al., “Numerical study of an
airfoil with riblets installed based on large eddy simulation”, Aerospace Science and Technology, 2018, 78:
661-670
21)Song,
W., Zhang, Y., Chen, H., “Design and Optimization of Multiple
Circumferential Casing Grooves Distribution Considering Sweep and Lean
Variations on the Blade Tip”, Energies, 2018, 11(9):
2401
22)Li,
R., Deng, K., Zhang, Y., Chen, H., “Pressure distribution guided
supercritical wing optimization”, Chinese
Journal of Aeronautics, 2018, 31(9):1842-1854.
23)Li,
S., Zhang, Y., Chen, H., et al., “Aerodynamic Optimization of
Turbine Based Combined Cycle Nozzle”, International
Journal of Turbo & Jet-Engines,
2018, 35(4):385-394
24)Zhang,
Y., Chen, H., Kan, W, et al., “Aeroacoustic Prediction
of a Multi-Element Airfoil Using Wall-Modeled Large-Eddy Simulation”, AIAA Journal, 2017, 55(12):
4219-4233.
25)Chen,
H., LI, Z., Zhang, Y., “U or V Shape: Dissipation Effects on
Cylinder Flow Implicit Large-Eddy Simulation”, AIAA Journal, 2017, 55(2): 459-473
26)Zhao,T., Zhang,
Y., Chen, H., et al., “Supercritical wing design based on airfoil
optimization and 2.75D transformation” , Aerospace Science and Technology, 2016, 56: 168-182
27)Li,
Z., Chen, H., Zhang, Y., Fu, S., “Grid-Convergence Study of
Two-Dimensional Euler Solutions”, Journal
of Aircraft, 2016, 53(1): 294-298
28)Zhang,
Y., Chen, H., Fu Song, et al. “Drag prediction
method of powered-on civil aircraft based on thrust drag bookkeeping”, Chinese Journal of Aeronautics, 2015, 28(4):
1023-1033
29)Li,
Z., Zhang, Y., Chen, H., “A low dissipation numerical scheme
for Implicit Large Eddy Simulation”, Computers
& Fluids, 2015, 117: 233-246
30)Zhang,
Y., Chen, H., Zhang, M., et al., “Performance
Prediction of Conical Nozzle Using
Navier–Stokes Computation”, Journal of Propulsion and Power, 2015.2, 31(1): 192~203.
31)Zhang,
Y., Fang, X., Chen, H., Fu, S., et al., “Supercritical
natural laminar flow airfoil optimization for regional aircraft wing
design”, Aerospace Science and
Technology, 2015, 43: 152-164
32)Xu,
K., Zhang, Y., Chen, H., et al., “The effects of vortex
breakdown on the static rolling aerodynamics of finned slender body”, Science China Physics,Mechanics &
Astonomy, 2014, 57(11): 2174-2176
33)Zhang,
Y., Chen, H., Fu S., “A Karman-Vortex Generator for
Passive Separation Control in a Conical Diffuser”, SCIENCE CHINA Physics, Mechanics & Astronomy, 2012, 55(5):
828-836.
34)Zhang,
Y., Chen H., Fu S., “Improvement to Patched Grid with
High-order Conservative Remapping Method”, Journal of Aircraft, 48(3): 884-893, 2011.
35)Xiao,
Z., Zhang, Y., Huang, J., et al., “Prediction of Separation Flows around
a 6:1 Prolate
Spheroid using RANS/LES Hybrid Approaches”, Acta Mechanica Sinica, 2007, 23(4):369-382.
36)Xiao,
Z., Chen, H., Zhang, Y., et al., “Study of delayed-detached
eddy simulation with weakly nonlinear turbulence model”, Journal of Aircraft, 2006, 43(5):
1377-1385.
37)李浩然, 李亚坤, 张宇飞, 陈海昕, CHN-T1标模的数值计算及气动特性研究, 空气动力学报, online.
38)张宇飞, 陈海昕, 方晓明, 基于CFD的涡扇发动机推阻分解方法及应用, 空气动力学学报, 2018, (03): 470-479 .
39)李润泽，张宇飞，陈海昕, "人在回路"思想在飞机气动优化设计中演变与发展, 空气动力学报，2017(04):529-543.
40)李钊, 陈海昕, 张宇飞, 基于k-kL两方程湍流模式的尺度自适应模拟, 工程力学, 2016.12.1, 33(12): 21-30.
41)张宇飞，刘瑞环，邓烨明，陈海昕，Meng Wang, 基于非定常流动模拟和FW-H方程的多段翼型噪声研究, 2016年度全国气动声学学术会议, 北京, 2016.11.04-2016.11.06.
42)张宇飞，刘瑞环，邓烨明，陈海昕，Meng Wang, 基于非定常CFD模拟和FW-H方程的气动噪声研究, 2015年度航空声学分会工作会暨全国气动声学学术会议, 哈尔滨, 2016.01.21-2016.01.23.
43)张宇飞，陈海昕，Meng Wang, 基于壁面模型大涡模拟的多段翼型噪声研究, 第九届全国流体力学学术会议, 南京市, 2016.10.21-2016.10.23.
44)李钊, 陈海昕, 张宇飞, 基于广义Richardson外插方法的阻力预测精度分析, 航空学报, 2015.1.26, 36(7): 2105-2114 .
45)赵童, 张宇飞, 陈海昕, 陈迎春, 张淼, 面向三维机翼性能的超临界翼型优化设计方法, 中国科学:物理学 力学 天文学,2015.10.20, (10): 89-101.
46)倪昂修, 张宇飞, 陈海昕, NSGA-Ⅱ算法的改进及其在多段翼型缝道参数优化中的应用, 空气动力学学报, 2014, (02): 252-257.
47)徐柯哲, 张宇飞, 陈海昕, 李斌, 刘仙名, 符松, 导弹大迎角下非线性诱导滚转力矩数值研究, 航空学报, 2014, (01): 97-104.
48)贾楠非, 张宇飞, 陈海昕, 考虑鲁棒性的超临界翼型激波控制鼓包减阻研究, 中国科学:物理学 力学 天文学, 2014, (03): 249-257.
49)续立军, 刘涛, 陈海昕, 张宇飞, 一种用于无人机姿态测量的红外地平仪算法改进, 中国惯性技术学报, 2014.8.15, (04): 474-480.
50)张文升, 陈海昕, 张宇飞, 陈迎春, 李亚林, 周涛, 短舱绕流片对运输机增升装置气动特性影响研究, 航空学报, 2013.1.1, 34(1): 76-85.
51)张宇飞, 陈海昕, 符松, 张淼, 张美红, 刘铁军, 一种实用的运输类飞机机翼/发动机短舱一体化优化设计方法, 航空学报, 2012 (11): 1993-2001.
52)张宇飞, 陈海昕, 符松, 基于高阶守恒重映对窗口嵌入技术的改进, 计算物理, 2011, (02): 167-173.
53)陈海昕, 张宇飞, 符松, 王薇, 大型客机前沿气动问题研讨会会议简介, 力学进展, 2009.1.25, (01): 120-122 .
54)张宇飞, 符松, 第五届国际计算流体力学大会介绍, 力学进展, 2008.9.25, (05): 652-652.
55)黎军, 张宇飞, 李天, 陈海昕, 操纵面偏转绕流数值研究, 空气动力学学报, 2008.9.15, (03): 384-387 .
56)张宇飞,肖志祥,符松, 流向强迫振荡圆柱绕流的涡脱落模态分析, 力学学报, 2007.5.15, 39(03): 408-416 .