All Stories

  1. Mach Number Effect on the Drag Reducing Performance of the Riblet in the Transition and Turbulent Flow

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

    Aiko Yakeno

  2. Experiments on the laminarization effect of Sinusoidal Roughness Elements on a swept wing.

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

    Sayaka Suzuki, Aiko Yakeno

  3. Traveling wave generation on a swept wing subjected to surface roughness and free-stream turbulence.

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

    Yuji Mori, Aiko Yakeno

  4. Flow control strategy for stably generating vortex

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

    Professor Kozo Fujii, Takuto Ogawa, Aiko Yakeno

  5. Drag reduction effect of distributed roughness on the transitional flow state using direct numerical simulation

    Article • International Journal of Heat and Fluid Flow, December 2023, Elsevier

    Aiko Yakeno

  6. Clear Air Turbulence Resolved by Numerical Weather Prediction Model Validated by Onboard and Virtual Flight Data

    Article • Geophysical Research Letters, June 2023, American Geophysical Union (AGU)

    Aiko Yakeno

  7. Propagation of stationary and traveling waves in a leading-edge boundary layer of a swept wing

    Article • Physics of Fluids, September 2021, American Institute of Physics

    Aiko Yakeno

  8. Drag reduction and transient growth of a streak in a spanwise wall-oscillatory turbulent channel flow

    Article • Physics of Fluids, June 2021, American Institute of Physics

    Aiko Yakeno

  9. Flow characteristics around extremely low fineness-ratio circular cylinders

    Article • Physical Review Fluids, May 2021, American Physical Society (APS)

    Aiko Yakeno

  10. Application of observability Gramian to targeted observation in WRF data assimilation

    Article • Tellus A Dynamic Meteorology and Oceanography, December 2019, Taylor & Francis

    Ryoichi Yoshimura, Aiko Yakeno

  11. 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

  12. Unsteady shear layer flow under excited local body-force for flow-separation control in downstream of a two-dimensional hump

    Article • International Journal of Heat and Fluid Flow, December 2018, Elsevier

    Aiko Yakeno

  13. Dominant parameters for maximum velocity induced by body-force models for plasma actuators

    Article • Theoretical and Computational Fluid Dynamics, October 2018, Springer Science + Business Media

    Professor Kozo Fujii, Aiko Yakeno

  14. Investigation of Maximum Velocity Induced by Body-Force Fields for Simpler Modeling of Plasma Actuators

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

    Aiko Yakeno

  15. Spanwise modulation effects of local body force on downstream turbulence growth around two-dimensional hump

    Article • International Journal of Heat and Fluid Flow, February 2017, Elsevier

    Professor Kozo Fujii, Aiko Yakeno

  16. Wall-Turbulence Structure with Pressure Gradient Around 2D Hump

    Article • January 2016, Springer Science + Business Media

    Professor Kozo Fujii, Aiko Yakeno

  17. Mechanisms for laminar separated-flow control using dielectric-barrier-discharge plasma actuator at low Reynolds number

    Article • Physics of Fluids, November 2015, American Institute of Physics

    Professor Kozo Fujii, Aiko Yakeno

  18. Multifactorial Effects of Operating Conditions of Dielectric-Barrier-Discharge Plasma Actuator on Laminar-Separated-Flow Control

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

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

  19. LES of Separated-flow Controlled by DBD Plasma Actuator around NACA 0015 over Reynolds Number Range of 10^4-10^6

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

    Dr Hikaru Aono, Professor Kozo Fujii, Aiko Yakeno

  20. LES on Turbulent Separated Flow around NACA0015 at Reynolds Number 1,600,000 toward Active Flow Control

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

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

  21. Plasma Flow Control Simulation of an Airfoil of Wind Turbine at an Intermediate Reynolds Number

    Article • July 2013

    Professor Kozo Fujii, Aiko Yakeno