All Stories

  1. High Enthalpy Effects on Hypersonic Boundary Layer Transition

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

    Hideyuki Tanno, Tony Liang, Jan-Erik Brune

  2. Operating Characteristics of Cylindrical Rotating Detonation Engines Using Liquid Ethanol and Liquid Nitrous Oxide

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

    Tomoki Sato, Director Masaharu Uchiumi, Ikkoh Funaki, Hideyuki Tanno, Jiro Kasahara

  3. Hayabusa2 SHARC Spectro-Radiometric Calibration and Analysis

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

    Hideyuki Tanno, Dr. Dinesh K. Prabhu, Christopher Johnston

  4. Comparison of flight and shock tunnel spectroscopy of Hayabusa2 Sample Return Capsule

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

    Hideyuki Tanno

  5. Analysis of Surface Temperature of Hayabusa1 & 2 SRC in Airborne Spectroscopy Measurement

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

    Hideyuki Tanno

  6. Aerodynamic measurements of a blunt cone with a high angle of attack in HIEST

    Article • November 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Hideyuki Tanno

  7. Aeroheating Measurement of HAYABUSA-CAPSULE using HEK-X Expansion Tube

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Hideyuki Tanno

  8. Flow Visualization inside a Rotating Detonation Engine near Injection Nozzles Using Point-Diffraction Interferometry

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Hideyuki Tanno

  9. Characterization of Radiative Heating Anomaly in High Enthalpy Shock Tunnels

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Hideyuki Tanno

  10. Experimental Investigation of Roughness Effects on Transition on Blunt Spherical Capsule Shapes

    Article • Journal of Spacecraft and Rockets, March 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Hideyuki Tanno, Rolf Radespiel

  11. High-Enthalpy Effects on Hypersonic Boundary-Layer Transition

    Article • Journal of Spacecraft and Rockets, March 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Hideyuki Tanno, Heath Johnson

  12. Analysis of Second-Mode Amplitudes on Sharp Cones in Hypersonic Wind Tunnels

    Article • Journal of Spacecraft and Rockets, March 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Hideyuki Tanno, Rolf Radespiel

  13. DNS of Interactions Between Low-Frequency Waves and Second Mode in Hypersonic Boundary Layer Transition

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

    Hideyuki Tanno

  14. High-speed visualization for test-time evaluation of a JAXA HEK-X free-piston driven expansion tube

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

    Hideyuki Tanno, Kohei Shimamura

  15. Numerical Study of Unsteady High Enthalpy Flow in an Expansion Tube

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

    Hideyuki Tanno

  16. Development of Free Flight Experimental and Analytical Procedures for Atmospheric Entry Vehicles

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

    Hideyuki Tanno, Olaseinde Jegede

  17. Analysis of Unstable Mode Structures in Hypersonic Boundary Layer

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

    Hideyuki Tanno

  18. Global Heat Flux Measurement Using Temperature-Sensitive Paint in High-Enthalpy Shock Tunnel HIEST

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

    Hideyuki Tanno

  19. Resonant growth of surface pressure fluctuation in hypersonic boundary layer in shock tunnel

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

    Hideyuki Tanno

  20. Aerodynamic Characteristics of Lifting Body HYFLEX under High-Temperature Real-Gas Conditio

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

    Hideyuki Tanno

  21. Porous Injection Effect on Surface Heat Flux in High-enthalpy High-Reynolds number flow

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

    Hideyuki Tanno

  22. Basic characteristics of the free-piston driven expansion tube JAXA HEK-X

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

    Hideyuki Tanno

  23. Visualization of Hypersonic Boundary Layer Transition on Elliptic Cone in High Enthalpy Shock Tunnel with Temperature-Sensitive Paint

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

    Hideyuki Tanno

  24. Global stability analysis on cone models under the conditions of the HIEST experiments

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

    Hideyuki Tanno

  25. Computation of Turbulent Heat Flux with Roughness Induced Transition in High Enthalpy Shock Tunnel HIEST

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

    Prof. Keisuke Sawada, Hideyuki Tanno

  26. Experimental Study of High-Enthalpy Heat Flux Augmentation in Shock Tunnels

    Article • Journal of Thermophysics and Heat Transfer, October 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Hideyuki Tanno

  27. Free-flight aerodynamic test of elliptic cone in Shock Tunnel

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

    Hideyuki Tanno

  28. Measurement of Ultraviolet Radiative Heating Augmentation in HIEST Reflected Shock Tunnel

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

    Hideyuki Tanno

  29. Radiative Heat Flux from Metallic Species in Free Piston Shock Tunnel HIEST

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

    Dr. Kazuhisa FUJITA, Hiroki Takayanagi, Hideyuki Tanno

  30. Boundary Layer Transition and Trip Effectiveness on an Apollo Capsule in the JAXA High Enthalpy Shock Tunnel (HIEST) Facility

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

    Hideyuki Tanno

  31. LES Computation of Turbulent Heat Flux on Reentry Capsule Afterbody with Forced Transition

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

    Hideyuki Tanno

  32. Aerodynamic Evaluation of a Capsule Shaped Projectile during Free Flight Testing with Ballistic Range

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

    Hideyuki Tanno

  33. Spectroscopic Investigation on Anomalous Heating in Free Piston Shock Tunnel HIEST

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

    Dr. Kazuhisa FUJITA, Hiroki Takayanagi, Hideyuki Tanno

  34. Experimental Study on Heat Flux Augmentation in High-enthalpy Shock Tunnels

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

    Prof. Keisuke Sawada, Hideyuki Tanno

  35. Free-flight aerodynamic tests of reentry vehicles in high-temperature real-gas flow (Invited)

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

    Hideyuki Tanno

  36. Aeroheating measurement of Apollo shaped capsule with boundary layer trip in the free-piston shock tunnel HIEST

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

    Hideyuki Tanno

  37. Numerical Analysis on Aerothermodynamic Characteristics of Blunt-nosed Cone in Free-piston Shock Tunnel HIEST

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

    Prof. Keisuke Sawada, Hideyuki Tanno