Aerospace Systems Engineering Research Center


Post:Associate Professor

Office Phone:021-34207065

Office Address:Room A337, Aerospace Building


Professional experience

Time Office Units Post
06/08 – present Shanghai Jiao Tong University Associate Professor
09/17-12/17 Hong Kong University of Science and Technology Visiting Associate Professor
2014-2017 University of Southampton Visiting Researcher
10/02 – 06/08 University of Southampton Research Fellow

Educational background

Time Graduated School Educational background
2002 Computational Engineering, University of Southampton, UK Ph.D.
1996 Structural Engineering, China Academy of Launch Vehicle Technology MSc.
1993 Flight Vehicle Design, Beihang University BSc.

Research Interests

  • Developed and continues to direct the Value-driven aircraft design with industrial partners
  • Developed high-order numerical methods for flow and acoustic analysis with applications to low noise highlift, contra-rotating open rotor configurations as well as engine nacelle acoustic liner optimizations
  • Developed efficient optimization methodology based on hybrid surrogate models and memetic optimization methods
  • Developed a framework for rapid aircraft sizing based on a variety of models
  • In parallel, conducted research in CFD and multi-disciplinary design optimization with applications to civil aircraft, amphibian

Selected publications

  1. Qiu, S., Song, W., Turbofan Duct Geometry Optimization for Low Noise Using Continuous Adjoint Method, to the 19th AIAA/CEAS Aeroacoustics Conference (34th AIAA Aeroacoustics Conference), 2013.
  2. Qiu, S., Song, W., Liu, H., Shape optimization of a general bypass duct for tone noise reduction using continuous adjoint method, Journal of Mechanical Engineering Science, Vol. 228, No. 1, pp. 119-134. 2015.
  3. Yiming Xu, Wenbin Song, Conceptual Design of a Submersible Aircraft with Morphing Technology, Asian Workshop on Aircraft Design Education, AWADE 2016, Nanjing, 2016.
  4. Xu Y, Song W, Zhao D. Efficient Optimization of Ringlets for Drag Reduction over the Complete Mission Profile [J]. AIAA Journal. 2018: 1-12.

Copyright© 2015 School of Aeronautics and Astronautics Email:

Technical Support: WeiCheng