All Stories

  1. Development of 3D Flow Analysis Method for Multicopter Rotors by Combination of Blade Element Theory and Actuator Line Model

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Hiroyuki Kato, Makoto Ueno

  2. Study on wind tunnel automation with flow velocity control and anomaly detection

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

    Hiroyuki Kato

  3. Numerical Assessment for PIV Measurement in Airplane Wakes

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

    Kisa Matsushima, Hiroyuki Kato

  4. Normalization of Wind-Tunnel Data for NASA Common Research Model

    Article • Journal of Aircraft, September 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Hiroyuki Kato, Makoto Ueno

  5. Towards EFD/CFD Integration: Development of DAHWIN - Digital/Analog-Hybrid Wind Tunnel

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Hiroyuki Kato