All Stories

  1. Effect of a streamwise vortex on supersonic boundary layer transition

    Article • Physics of Fluids, March 2023, American Institute of Physics

    Weidong Liu

  2. Flow structures of strong interaction between an oblique shock wave and a supersonic streamwise vortex

    Article • Physics of Fluids, October 2022, American Institute of Physics

    Weidong Liu

  3. Structural characteristics of the strong interaction between oblique shock wave and streamwise vortex

    Article • Physics of Fluids, October 2022, American Institute of Physics

    Weidong Liu

  4. Flowfield Analysis and Reconstruction of Ethylene–Air Continuous Rotating Detonation Wave

    Article • AIAA Journal, February 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Weidong Liu

  5. Ethylene Continuous Rotating Detonation in optically accessible racetrack-like combustor

    Article • Combustion Science and Technology, July 2018, Taylor & Francis

    Weidong Liu

  6. Experimental Investigation on Fuel Distribution in a Scramjet Combustor with Dual Cavity

    Article • Journal of Propulsion and Power, March 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Weidong Liu, Li XIPENG

  7. A study of the asymmetric shock reflection configurations in steady flows

    Article • Journal of Fluid Mechanics, July 2017, Cambridge University Press

    Weidong Liu

  8. Effect of Microramp on Transverse Jet in Supersonic Crossflow

    Article • AIAA Journal, December 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Weidong Liu

  9. ignition process in scramjet combustors

    Article • Journal of Propulsion and Power, March 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Li XIPENG, Weidong Liu