All Stories

  1. Dynamic Stall Control Using Spanwise-Type and Vortex-Generator-Type Plasma Actuators Around Pitching Airfoil

    Article • July 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Makoto Sato

  2. Large-Eddy-Simulations on Dynamic Stall Control Using Plasma Actuators at Reynolds Number of 1.0×106

    Article • July 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Makoto Sato

  3. Numerical Investigation on Interaction Between Wing and Propeller Installed in Close Proximity to Both Upper and Lower Surfaces of Wing

    Article • July 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Makoto Sato

  4. Numerical investigation on streamwise vortex generation by plasma actuator

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

    Makoto Sato

  5. Numerical Analysis on Hovering Performance of Hexacopter “HAMILTON” for Mars Exploration

    Article • June 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Masahiro Kanazaki, Makoto Sato

  6. Virtual vortex generator

    Article • June 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Makoto Sato

  7. Unified mechanisms for separation control around airfoil using plasma actuator with burst actuation over Reynolds number range of 103–106

    Article • Physics of Fluids, February 2020, American Institute of Physics

    Makoto Sato

  8. Mechanisms for turbulent separation control using plasma actuator at Reynolds number of 1.6 × 106

    Article • Physics of Fluids, September 2019, American Institute of Physics

    Dr Hikaru Aono, Professor Kozo Fujii, Taku Nonomura, Makoto Sato, Aiko Yakeno