All Stories

  1. Numerical study on the influence of inlet cover opening process on the stage transition performance of solid propellant ducted rockets

    Article • Physics of Fluids, July 2025, American Institute of Physics

    zhiwen wu

  2. Direct thrust test and asymmetric performance of porous ionic liquid electrospray thruster

    Article • Chinese Journal of Aeronautics, April 2023, Tsinghua University Press

    zhiwen wu

  3. Interaction between electrospray using ionic liquid and simultaneous corona discharge under positive and negative polarity

    Article • Physics of Plasmas, July 2019, American Institute of Physics

    zhiwen wu

  4. Parametric Study of an Air-Breathing Electric Propulsion for Near-Space Vehicles

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

    zhiwen wu

  5. Optimization of the Energy Distribution in Ablative Pulsed Plasma Thrusters

    Article • AIAA Journal, August 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Guorui Sun, zhiwen wu

  6. Maximum Thrust of Single Dielectric Barrier Discharge Thruster at Low Pressure

    Article • AIAA Journal, June 2018, American Institute of Aeronautics and Astronautics (AIAA)

    zhiwen wu

  7. Influence and efficiency of energy harvesting on the process of de-orbiting using bare electrodynamic tether system

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

    zhiwen wu

  8. Numerical Investigation of Self-Ignition Characteristics of Solid-Fuel Scramjet Combustor

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

    zhiwen wu

  9. Numerical and Experimental Study on the Solid-Fuel Scramjet Combustor

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

    zhiwen wu

  10. Plume Structure and Current-Voltage Characteristic Analysis for a Cathodic Plasma Contactor

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    zhiwen wu