Associate Professor
Cell phone: 15827475204
Email: jiewu@hust.edu.cn
Academic Areas: Aerodynamics
Research Interests: Hypersonic flow, experimental fluid dynamics, wind tunnel technologies, jet noise and control, CFD application
Academic Degrees
PhD in Fluid mechanics, 2015, Technische Universität Braunschweig, Germany
Professional Experience
2015.05-2016.9, Research fellow, Nanyang Technological University, Singapore
2017.11~2018.9,DAAD research associate, Technische Universität Braunschweig, Germany(sponsered by DAAD)
2016.9~present, Associate Professor, Huazhong University of Science and Technology, China
Selected Publications
[1]. Wu J, H. D. Lim,Wei X.F, New Thz How and Cui Y.D. Flow characterization of supersonic jets issuing from double-bevelled nozzles. Journal of Fluids Engineering. 2019, Volume 141.
[2]. Wu J and Radespiel R. Damping insert materials for settling chambers of supersonic wind tunnels. Experiments in Fluids. 2017. Volume 58, Issue 3: 19-27. (DOI: 10.1007/s00348-017-2310-5)
[3]. 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)
[4]. 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)
[5]. 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）
[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)
Courses Taught
Fundamentals of aerodynamics, Experimental fluid mechanics
Project
NSFC(2017-2019) Disturbance characterization of freestream in hypersonic wind tunnels;
Awards
None
