副教授

吴杰

作者: 时间:2017-07-04 点击数:

            


               姓 名:吴杰

                称:副教授

               电 话:027-87540185

               电子邮箱:jiewu@hust.edu.cn

                                              




主要经历

2005 – 2009,西北工业大学航空学院飞行器环境和生命保障工程专业,学士;

2009 – 2011,西北工业大学航空学院飞行器设计专业,硕士;

2010 – 2015,德国布伦瑞克工业大学流体力学系,工学博士;

2015 – 2016,新加坡南洋理工航空工程系,博士后;

2016 – 至今,华中科技大学航空航天学院,副教授。

科学研究方向

l 实验流体力学(新型测量方法开发、流体现象观测)

l 超声速风洞设计及风洞实验与测量

l 超声速/高超声速空气动力学(超声速及高超声速飞行器设计)

l 超声速喷流测量及噪声控制(战斗机/火箭发动机的流场/声场)

l CFD 应用及开发

项目经验

[1] 先进风洞气动设计技术,总装,315万,在研

[2] 高超声速风洞中来流扰动模态特征的研究,国家自然基金青年项目,31万,在研

[3] 三维纹影仪在超声速喷流测量中的应用研究及噪声机理研究,南洋理工大学航空工程学院,新加坡, 20152016

[4] 大型低速风洞数值模拟,布伦瑞克工业大学推进与涡轮机械所,德国,2014~2015

[5] 超声速流动下尖锥体表面不稳定波的增长机理研究, 布伦瑞克工业大学流体力学所,德国,2012~2014

[6] 超声速风洞的动态响应分析及流场品质提高设计,布伦瑞克工业大学流体力学所,德国,2013~2014

[7] 高超声速风洞流场动态响应的标定及流场扰动的演化,布伦瑞克/亚琛工业大学流体力学所,德国,2013~2014

[8] 串列式Ma 3 超声速风洞流场校核,布伦瑞克工业大学流体力学所,德国,2012~2013

[9] 串列式Ma 3超声速风洞设计, 布伦瑞克工业大学流体力学所,德国,2011~2012

开设课程

l 空气动力学

l 流体/固体力学实验

l 可压缩空气动力学

l 气动声学基础

代表成果

专著

[1] Jie Wu. Boundary-layer Instability Experiments in a Tandem Nozzle Supersonic Wind Tunnel. ISBN: 978-3-8440-3522-3. March, 2015. SHAKER VERLAG, Germany.(DOI: 10.2370/9783844035223)

会议论文

[1] Lim, H.D., Wu, J., New,T.H and Shi,Shengxian. 2017. Challenges of Optical Flow Analysis in Supersonic Jets. 55th AIAA Aerospace Sciences Meeting, Texas.

[2] Wu, J. 2014. Aerodynamic Design and Analysis of a Supersonic Wind Tunnel with Tandem Nozzle. Proceedings of the 2nd NPU-DLR Workshop on Aerodynamics at Germany, Braunschweig.

[3] Ali, S.R.C., Wu, J., Radespiel,R., Schilden,T and Schröder, W. 2014. High-Frequency Measurements of Acoustic and Entropy Disturbances in a Hypersonic Wind Tunnel. In: 44th AIAA Fluid Dynamics Conference. Atlanta.

[4] Wu, J and Radespiel, R. 2013. Experimental Investigation of a Newly Designed Supersonic Wind Tunnel. In: 5th European conference for aeronautics and space sciences. Munich.

[5] Wu, J and Radespiel, R. 2012. Tandem Nozzle Supersonic Wind Tunnel Design. In: Proceedings 47th International Symposium of Applied Aerodynamics. Paris.

期刊论文

[1] Wu J and Radespiel R. Damping insert materials for settling chambers of supersonic wind tunnels. Experiments in Fluids. 2017. (DOI: 10.1007/s00348-017-2310-5)

[2] Wu J and New Thz How. An investigation on supersonic bevelled nozzle jets. Aerospace Science and Technology. 2017. Volume 63:278–293. (DOI:http://dx.doi.org/10.1016/j.ast.2017.01.003)

[3] Wu J, Liu X and Radespiel R. RANS simulations of a tandem nozzle supersonic wind tunnel. Aerospace Science and Technology. 2016. Volume 49: 215-224. (DOI:10.1016/j.ast.2015.11.041)

[4] Schilden T, Schröder W, Ali S.R.C, Schreyer A.M, Wu J, and Radespiel R. Analysis of Acoustic and Entropy Disturbances in a Hypersonic Wind Tunnel. Physics of Fluids. 2016. Volume.28, Issue 5, 056104.(DOI: http://dx.doi.org/10.1063/1.4948435

[5] Stephan S, Wu J, and Radespiel R. Propulsive Jet Influence on Generic Launcher Base Flow.  CEAS Space Journal. 2015: 1-21.(DOI: 10.1007/s12567-015-0098-9)

[6] Wu J and Radespiel R. Investigation of Instability Wave in a Mach 3 Laminar Boundary-layer. AIAA Journal. 2015. Volume 53, Issue 12: 3712-3725. (DOI: 10.2514/1.J054040)

[7] Wu J, Zamre P, Radespiel R. Flow Quality Experiment in a Tandem Nozzle Wind Tunnel at Mach 3. Experiments in Fluids. 2015. Volume 56, Issue 1: 1-18.(DOI: 10.1007/s00348-014-1887-1)

[8] Wu J and Radespiel R. 2015. Experimental Investigation of a Newly Designed Supersonic Wind Tunnel. Progress in flight physics. 2015. Volume 7. Page 123-144.(DOI: http://dx.doi.org/10.1051/eucass/201507123 )

[9] Wu J and Radespiel R. Tandem Nozzle Supersonic Wind Tunnel Design. International Journal of Engineering Systems Modelling and Simulation. 2013. Volume 5. Page 8-18.(DOI: 10.1504/IJESMS.2013.052369)


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