All Stories

  1. Experimental and Numerical Investigation of a Fluidically Variable Hypersonic Inlet

    Article • AIAA Journal, August 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Chen Hao, Huijun Tan, Dr Chenghong LI

  2. Influence of Secondary Flow Injection Angle on a Fluidic Shock Control Technique

    Article • Journal of Propulsion and Power, March 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Huijun Tan, Dr Chenghong LI