All Stories

  1. High-pressure hydrogen rocket engine system

    Article • Journal of Propulsion and Power, June 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Takeshi Kanda

  2. Mechanism of rotating detonation and its limit to rocket/jet engine application

    Article • Physics of Fluids, November 2024, American Institute of Physics

    Takeshi Kanda

  3. Turbulent-to-Laminar Reverse Transition

    Article • Scientific Reports, July 2023, Springer Science + Business Media

    Takeshi Kanda

  4. Study of High-frequency Combustion Instability of Liquid-Propellant Rocket Engines

    Article • Acta Astronautica, January 2023, Elsevier

    Takeshi Kanda

  5. Theoretical study of detonation

    Article • Physics of Fluids, July 2022, American Institute of Physics

    Takeshi Kanda

  6. Study of laminar-to-turbulent pipe flow transition

    Article • Physics of Fluids, March 2022, American Institute of Physics

    Takeshi Kanda

  7. Effect of Centrifugal Force on Gas Flow in a Supersonic Turbine

    Article • Journal of Engineering for Gas Turbines and Power, February 2022, ASME International

    Takeshi Kanda

  8. Study of High-frequency Combustion Instability of Liquid Rocket Engines

    Article • Acta Astronautica, January 2021, Elsevier

    Takeshi Kanda

  9. Experiment on Air Intake Performance of Ejector-Jet using Wax-based Fuel Hybrid Rocket.

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

    Takeshi Kanda

  10. Study of high-frequency combustion instability

    Article • TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, January 2019, Japan Society for Aeronautical and Space Sciences

    Takeshi Kanda

  11. Theoretical study of pipe flow transition

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

    Takeshi Kanda

  12. Conceptual study of radiative heating in rocket engine combustion chamber

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

    Takeshi Kanda

  13. Study of boundary layer transition

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

    Takeshi Kanda

  14. Theoretical study of boundary layer transition in supersonic flow

    Article • TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, January 2011, Japan Society for Aeronautical and Space Sciences

    Takeshi Kanda

  15. Conceptual study of aerospace plane with RBCC

    Article • Journal of Propulsion and Power, March 2007, American Institute of Aeronautics and Astronautics (AIAA)

    Takeshi Kanda

  16. Scramjet test at Mach 8 condition

    Article • Journal of Propulsion and Power, March 2006, American Institute of Aeronautics and Astronautics (AIAA)

    Takeshi Kanda

  17. Design of RBCC

    Article • October 2005, American Institute of Aeronautics and Astronautics (AIAA)

    Takeshi Kanda

  18. Study of aerospace plane with RBCC

    Article • Journal of Propulsion and Power, September 2003, American Institute of Aeronautics and Astronautics (AIAA)

    Takeshi Kanda