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  1. Research on the Flow Characteristics of DBD Plasma Actuation Based on High Speed Schlieren

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

    FENG LI

  2. The Effects of Mach Number Control Precision on Airfoil Pressure Measurement in a Transonic Wind Tunnel

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

    FENG LI

  3. Dynamic Characteristics of the Density Field near Wall Region Actuated by Plasma

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

    FENG LI

  4. The Phenomenology and Physics of Peristaltic Flow Acceleration Induced by Multiple DBD Plasma Actuators Based on PIV

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

    FENG LI