All Stories

  1. Unsteady Flow Field Around NACA0012 Airfoil Undergoing Constant Pitch Rates at Low Reynolds Numbers

    Article • June 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Hajime Itoh, Makoto Mizoguchi

  2. Potential of Glow-Discharge Flow Measurement in Hypersonic Low-Density Flows

    Article • AIAA Journal, January 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Hajime Itoh, Makoto Mizoguchi

  3. Spectral Measurements in Electrical Discharge Glow Plasma Produced in Hypersonic Separated Flow

    Article • January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Hajime Itoh, Makoto Mizoguchi

  4. Method for Visualizing Viscous Interaction in Hypersonic Low-Density Flows Using Electrical Discharge

    Article • Journal of Spacecraft and Rockets, January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Hajime Itoh, Makoto Mizoguchi

  5. Experimental Investigation of Aspect-Ratio-One Wing Characteristics at Low Reynolds Numbers

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

    Dr. Hajime Itoh, Makoto Mizoguchi

  6. Experiments on Unsteadiness Associated with Cylinder-induced Shock-Laminar Boundary Layer Interaction in Hypersonic Flow

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

    Dr. Hajime Itoh, Makoto Mizoguchi

  7. Stall hysteresis and aerodynamic characteristics of low-aspect-ratio wings

    Article • TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, January 2016, Japan Society for Aeronautical and Space Sciences

    Makoto Mizoguchi

  8. Static Stall Hysteresis of Low-Aspect-Ratio Wings

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

    Makoto Mizoguchi, Dr. Hajime Itoh

  9. Glow Discharge Visualization of Hypersonic Separated Flow

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

    Makoto Mizoguchi, Dr. Hajime Itoh

  10. Aerodynamic characteristics of bluff flat-plate wings at low Reynolds numbers

    Article • AIAA Journal, July 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Makoto Mizoguchi, Dr. Hajime Itoh

  11. Ramp Wall Pressure Measurement in Hypersonic Shock/Boundary Layer Interaction

    Article • June 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Makoto Mizoguchi, Dr. Hajime Itoh

  12. Effect of Aspect Ratio on Aerodynamic Characteristics of Rectangular Wings at Low Reynolds Numbers

    Article • January 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Makoto Mizoguchi, Dr. Hajime Itoh

  13. 低レイノルズ数流れにおける矩形平板翼の空力特性

    Article • JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, January 2012, Japan Society for Aeronautical and Space Sciences

    Makoto Mizoguchi

  14. Analytical model of free-piston motion including diaphragm opening for free-piston shock tunnels

    Article • Shock Waves, July 2009, Springer Science + Business Media

    Makoto Mizoguchi

  15. Influence of Coolant Gas Properties on Film Cooling Effectiveness in High Enthalpy Flows

    Article • January 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Makoto Mizoguchi

  16. Film Cooling Effectiveness in High Enthalpy Flows

    Article • JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, January 2007, Japan Society for Aeronautical and Space Sciences

    Makoto Mizoguchi

  17. フリーピストン衝撃風洞駆動部におけるピストン運動の数値解析

    Article • JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, January 2007, Japan Society for Aeronautical and Space Sciences

    Makoto Mizoguchi

  18. Numerical Study on Diaphragm Rupture for Performance Improvement of a Free Piston Shock Tunnel

    Article • November 2006, American Institute of Aeronautics and Astronautics (AIAA)

    Makoto Mizoguchi

  19. Reduction of Aerodynamic Heating with Wall Catalysis by Film Cooling

    Article • November 2006, American Institute of Aeronautics and Astronautics (AIAA)

    Makoto Mizoguchi

  20. A Study on Increase of Duration of a Free Piston Shock Tunnel

    Article • January 2004, American Institute of Aeronautics and Astronautics (AIAA)

    Makoto Mizoguchi

  21. On the Characteristics of an Electric Discharge Generated across a Shock Wave in a Hypersonic Flow

    Article • JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, January 2003, Japan Society for Aeronautical and Space Sciences

    Makoto Mizoguchi, Dr. Hajime Itoh