User:Swysailing
From CFD-Wiki
Wei-Yi SU Associate professor College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, China ADD: 29 Yudao St., Nanjing 210016, China Email: weiyi_su@nuaa.edu.cn
Research Interests My research interests are mainly on supersonic/hypersonic inlet aerodynamics, including the shock-wave/boundary layer interactions in the hypersonic inlet-isolator, the hypersonic inlet starting/unstart mechanism, fluid-combustion interaction and flow control. Also, I am very interested in CFD optimization, inverse design, and airframe/propulsion integration.
Education S.B., Northwestern Polytechnical University S.M., Northwestern Polytechnical University Master thesis: Numerical simulation of the internal flow field of electrical propulsion engine
PHD, Institute of Mechanics, Chinese Academy of Sciences PHD Thesis: Shock-wave/boundary layer interactions and MHD flow control.
Research Skills
-Pointwise gridgen grid generation
-Computational fluid dynamics based on multi-block structure grid RANS solver
-inlet design
-CFD optimization design based on Matlab or Isight
Professional experience Postdoctoral research, Nanjing University of Aeronautics and Astronautics, 2009-2011.
Lecturer, Nanjing University of Aeronautics and Astronautics, 2011-2013 Associate professor, Nanjing University of Aeronautics and Astronautics, 2013-present
Selected Publications • Wei-Yi Su, Kun-Yuan Zhang, "Back-Pressure Effects on the Hypersonic Inlet-Isolator Pseudoshock Motions," Journal of Propulsion and Power, Vol.29 (6), 2013, pp. 1391-1399. • Wei-Yi Su, Xin-Yu Chang, Kun-Yuan Zhang, "Effects of Magnetohydrodynamic Interaction-Zone Position on Shock-Wave/Boundary-Layer Interaction," Journal of Propulsion and Power, Vol.26 (5), 2010, pp. 1053-1058. • Wei-Yi Su, Kun-Yuan Zhang, Zhi-Guang Jin, " Inverse design of a curved wall compression hypersonic inlet based on Genetic Algorithms," Journal of Propulsion Technology(In China), Vol.32(5),2011,pp. 601-605. • Wei-Yi Su, Xin-Yu Chang, Kun-Yuan Zhang, " Numerical investigation of Lorentz force control on hypersonic inlet boundary layer separation," Journal of Propulsion Technology(In China), Vol.32(1),2011,pp. 36-41. • Wei-Yi Su, Kun-Yuan Zhang, Zhi-Guang Jin, " Investigation of a new-type passive control method on shock-wave/boundary layer interactions," Acta Aerodynamica Sinica (In China), Vol.29(6),2011,pp. 738-743. • Wei-Yi Su, Kun-Yuan Zhang, Zhi-Guang Jin, " Adaptive passive control on hypersonic inlet boundary layer separation," Journal of Propulsion Technology(In China), Vol.32(4),2011,pp. 455-460. • Wei-Yi Su, Lihong Chen, Xin-Yu Chang, "Physics and numerical simulations of MHD accelerated supersonic boundary layer," Chinese Journal of Theoretical and Applied Mechanics (In China), Vol.42 (4), 2010, pp. 782-788.
