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. Static Stall Hysteresis of Low-Aspect-Ratio Wings

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

    Makoto Mizoguchi, Dr. Hajime Itoh

  8. Glow Discharge Visualization of Hypersonic Separated Flow

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

    Makoto Mizoguchi, Dr. Hajime Itoh

  9. 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

  10. 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

  11. 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

  12. Reattaching Flow Visualization by Means of Glow Spark in Hypersonic Shock-Wave/Boundary-Layer Interaction

    Article • JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, January 2010, Japan Society for Aeronautical and Space Sciences

    Dr. Hajime Itoh

  13. A Simple Technique for Controlling the Görtler Vortex Wavelength in Hypersonic Shock-Wave/Boundary-Layer Interaction

    Article • JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, January 2010, Japan Society for Aeronautical and Space Sciences

    Dr. Hajime Itoh

  14. Effects of the Shape of a Separated Region in Hypersonic Shock-Wave/Boundary-Layer Interaction

    Article • JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, January 2008, Japan Society for Aeronautical and Space Sciences

    Dr. Hajime Itoh

  15. An Experimental Study on Unsteadiness of Hypersonic Separated Flow over a Compression Ramp

    Article • Journal of the Visualization Society of Japan, January 2008, The Visualization Society of Japan

    Dr. Hajime Itoh

  16. A Simple Prediction for the Location of High Aerodynamic Heating Region in Hypersonic Ramp Flows

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

    Dr. Hajime Itoh

  17. An Experimental Study on a Ramp-Induced Shock-Wave/Transitional-Boundary-Layer Interaction in Hypersonic Flow

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

    Dr. Hajime Itoh

  18. Study on Hypersonic Compression Corner Flows Using Glow Discharge-Tracer Technique

    Article • JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, January 2006, Japan Society for Aeronautical and Space Sciences

    Dr. Hajime Itoh

  19. Behaviour of Hypersonic Flow past a Control Flap

    Article • Journal of the Visualization Society of Japan, January 2005, The Visualization Society of Japan

    Dr. Hajime Itoh

  20. Glow Discharge-Tracer Technique for Velocity Profile Measurement in Hypersonic Boundary Layer Flows

    Article • JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, January 2005, Japan Society for Aeronautical and Space Sciences

    Dr. Hajime Itoh

  21. Visualization of Velocity Fields around Hypersonic Compression Corner Flows

    Article • Journal of the Visualization Society of Japan, January 2004, The Visualization Society of Japan

    Dr. Hajime Itoh

  22. 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

  23. On the Shock Wave Visualization in Hypersonic Flows Using Glow Discharge

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

    Dr. Hajime Itoh

  24. Visualization of Viscous Hypersonic Flow Using a Spark Technique.

    Article • Journal of the Visualization Society of Japan, January 1999, The Visualization Society of Japan

    Dr. Hajime Itoh

  25. An Experimental Investigation of Shock-Wave Boundary-Layer Interaction in Hypersonic Flow

    Article • Journal of the Visualization Society of Japan, January 1999, The Visualization Society of Japan

    Dr. Hajime Itoh

  26. Visualization of Hypersonic Separated Flow by Afterglow Technique.

    Article • TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B, January 1997, Japan Society of Mechanical Engineers

    Dr. Hajime Itoh

  27. Visualization of Viscous Hypersonic Flow Using a Spark Technique

    Article • Journal of the Visualization Society of Japan, January 1997, The Visualization Society of Japan

    Dr. Hajime Itoh

  28. Development of a Diaphragmless shock Tunnel Using a Butterfly Valve.

    Article • TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B, January 1997, Japan Society of Mechanical Engineers

    Dr. Hajime Itoh

  29. やや鈍い先端を有する平板周りの極超音速粘性流れ場における迎え角の影響

    Article • January 1996, Japan Society for Aeronautical and Space Sciences

    Dr. Hajime Itoh

  30. A Study on Shock Tube Flow with Energy Loss at the Diaphragm Section.

    Article • The Journal of the Japan Society of Aeronautical Engineering, January 1996, Japan Society for Aeronautical and Space Sciences

    Dr. Hajime Itoh