Expertise

Areas of Research:

  • High-Order Numerical Solvers
  • Hypersonic Boundary Layers
  • Shock – Turbulence Interaction
  • Flow – Structure Interaction
  • Advanced Propulsion System

Dr. Xiaowen Wang’s research interests include high-order numerical methods, CFD of thermochemical non-equilibrium flows, stability analysis and transition control of hypersonic boundary layers, direct numerical simulation of shock and turbulence interaction.

Communities
Aerospace Engineering
Degrees
PhD, University of California, Los Angeles, Mechanical Engineering, 2007
MS, University of Science and Technology of China, China, Fluid Mechanics, 2002
BS, University of Science and Technology of China, China, Theoretical and Applied Mechanics, 1999