中国·3044AM永利集团(股份)有限公司-官方网站

Faculty
WANG Xiaoliang
WANG Xiaoliang
Associate Researcher
School of Aeronautics and Astronautics, Room 327 wangxiaoliang@sjtu.edu.cn

Educational Background

  • 2003 - 2006， Shanghai Jiao Tong University, China, Doctor
  • 2000 - 2003， Taiyuan University of Technology, Master
  • 1994 - 1998， Taiyuan University of Technology, Bachelor

Work Experience

  • 2011-Present，Shanghai Jiao Tong University，Associate Professor
  • 2006-2011，Shanghai Jiao Tong University，Assistant Research Fellow

Research Interests

  • Calculation aerodynamics and application
  • Fluid-Structure couple computation and application
  • Flight mechanics and control law design of rigid and flexible aircraft (large passenger aircraft and airship)
  • Active and passive flow control design technology
  • Aircraft parametric modeling, sensitivity analysis and optimization design
  • Surrogate model of aerodynamics of parametric aircraft using high fidelity simulations and Neural Network

Representative Papers And Monographs

  • Xiao-liang WANG, Fu-xin WANG and Ya-lin Li, “Aerodynamic Characteristics of High-Lift Devices with Downward Deflection of Spoiler,” Journal of Aircraft, Vol.48, No.2, pp.730-735, 2011.
  • Mao-hua Zhang,Xiao-liang Wang* and Deng-ping DUAN.Panel method Predictions of Added Mass for Flexible Airship,The Aeronautical Journal,Volume 117,Number 1191,2013,pp519-531.
  • Xiao-liang WANG*,“Effect of Ballonet Sloshing on the Stability Characteristics of an Airship,” AIAA Journal, Vol.54,pp.360-364, 2016.
  • Ding Han, Xiao-liang Wang*, Lin Yan, Guozheng Yan, and Dengping Duan."Investigation of Airship Motion Sensitivity to Geometric Parameters", 55th AIAA Aerospace Sciences Meeting, AIAA SciTech Forum, 2017.
  • Wei-Cheng Xie, Xiao-Liang Wang, Deng-Ping Duan and Ji-Wei Tang,Finite Element Simulation of the Microstructure of Stratospheric Airship Envelopes, AIAA Journal Vol 58, Issue 8.2020, pp3690-3699.
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