国際会議Proceedings - 湊　亮二郎

1. Metal Particle Damper Characteristics for Gas-Generator Cycle Air Ramjet Engine

   1. Minato, R., Sasaki, H., Nakata, D. and Uchiumi, M.，25th International Society of Air Breathing Engine，2022年09月

   

2. Study of Low-Speed Aerodynamic Performance of a Supersonic Intake

   Ryo Kanbara, Ryojiro Minato, Daisuke Nakata，Proceedings of ISABE 2024，2024年09月，トゥールーズ（フランス）

   

3. Application and Testing of Nitromethane Monopropellant From Rocket to Air-Breathing Engine

   Ryojiro Minato, Daisuke Nakata, Shuichi Nakamura, Kazuyuki Higashino，Proceedings of ISABE 2024，2024年09月，トゥールーズ（フランス）

   

4. Turbine Supply Gas Temperature Equalization in a Gas Generator Cycle Air Turbo Ramjet Engine

   Daisuke Nakata, Akimoto Fujiura, Mio Namera, Naoki Hanawa, Ryojiro Minato, Hikaru Eguchi, Masaharu Uchiumi，Proceedings of ISABE 2024，2024年09月，トゥールーズ（フランス）

   

5. Dual Manifold Flow Control System for Gas-Generator Cycle Air Ramjet Engine

   Ryojiro Minato, Daisuke Nakata, Masaharu Uchiumi, Inaho, Yoshikawa, Hiromitsu, Yagihashi and Kouki Arimatsu，24th International Society of Air Breathing Engine，2019年09月，Canberra, Australia

   

6. Hot Gas Temperature Distribution in a Gas-Generator for Air Turbo Ramjet Engine

   Daisuke Nakata, Ryojiro Minato, Hiromitsu Yagihashi, Koki Arimatsu, Inaho Yoshikawa, Satoshi Inazumi, Masaya Sumiyoshi, Masaharu Uchiumi，24th International Society of Air Breathing Engine，2019年09月，Canberra, Australia

   

7. Experimental Study of Temperature and Phase Transition of Liquid Oxygen at Ignition in Impinging Injector of Gas Generator

   Hiromitsu Yagihashi, Daisuke Nakata, Ryojiro Minato, Inaho Yoshikawa, Koki Arimatsu, Masaharu Uchiumi，ASME-JSME-KSME 2019 Joint Fluids Engineering Conference AJKFLUIDS2019，American Society of Mechanical Engineering，2019年07月，San Francisco

   

8. The Minimum Flow Rate of Liquid Oxygen when Considering a Throttling of a Gas Generator Cycle Engineof

   Daisuke Nakata, Ryojiro Minato, Inaho Yoshikawa, Hiromitsu Yagihashi, Koki Arimatsu and Masaharu Uchiumi，ASME-JSME-KSME 2019 Joint Fluids Engineering Conference AJKFLUIDS2019，American Society of Mechanical Engineering，2019年07月，San Francisco

   

9. On the Pressure Loss Characteristics of Liquid Oxygen Considering a Heat Input

   Koki Arimatsu, Daisuke Nakata, Ryojiro Minato, Inaho Yoshikawa, Hiromitsu Yagihashi, Masaharu Uchiumi，32nd International Symposium on Space Technology and Science，The Japan Society of Aeronautical and Space Science，2019年06月，福井

   

10. Analytical and Experimental Study of Compressor Performance for Gas Generator Cycle Air Turbo Ramjet Engine

    Ryojiro Minato, Ryoji Imai, Kazuyuki Higashino, Daisuke Nakata, Mayu Ishihara，International Society of Air Breathing Engine，Article Number:ISABE 2017 22624，2017年09月，Manchester (UK)

    

11. Sea Level Static Tests of Gas Generator Cycle Air Turbo Ramjet Engine for Supersonic UAV

    Kazuyuki Higashino, Daisuke Nakata, Ryojiro Minato, Ryoji Imai, Nobuhiro Tanatsugu, Yuta Yashima and Hiroto Mukae，International Society of Air Breathing Engine，Article Number:ISABE 2017-22623，2017年09月

    

12. Design and Development of Bio-Ethanol Fueled GG-cycle Air Turbo Ramjet Engine for Supersonic UAV

    Ryojiro Minato, Kazuyuki Higashino, Nobuhiro Tanatsugu，ISABE 2013，Article Number:ISABE 2013-1654，2013年09月，韓国　釜山

    

13. Design and Performance Analysis of Bio-Ethanol Fueled GG-cycle Air Turbo Ramjet Engine

    Minato, Higashino, K., Tanatsugu, N.，AIAA Science Meeting 2012，AIAA Paper 2012-0842巻，AIAA，2012年01月，Nashville

    

14. Development Study on Counter Rotating Fan Jet Engine for Supersonic Flight

    Minato,　Ｒ., Kato, D., Higashino, K., Tanatsugu, N.，20th International Symposium of Air Breathing Engine，ISABE 2011-1233巻，AIAA，2011年09月，Gotenburg

    

15. LNG Rocket Engine with Coking Inhibited Regenerative Cooling System

    Minato,R., Higashino,K., Sugioka, M., Kobayashi,T., Ooya,S., Sasayama, Y.，16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference，AIAA-2009-7392巻，AIAA，2009年10月，Bremen

    

16. Study of Subscale Turbojet Engine for Supersonic Unmanned Plane in Muroran Institute of Technology

    Minato, R，International Symposium of Advanced Engineering，釜慶大学校，2009年03月，釜山

    

17. Development of a Design Support System that can Efficiently Utilize Non-Dominated Solutions

    Watanabe, S. and Minato, R.，Joint 4th International Conference on Soft Computing and Intelligent Systems and. 9th. International Symposium on advanced Intelligent Systems，2008年，名古屋

    

18. Development of Counter Rotating Axial Fan Turbojet Engine for Supersonic Unmanned Plane at Muroran Institute of Technology

    Minato, R., Himeno, T., Kojima, T., Kobayashi, H., Taguchi, H., Tetsuya Sato, T., Arai, T., Mizobata, K., Sugiyama, H., Tanatsugu, N，International Gas Turbine Congress , Tokyo, 2007，日本ガスタービン学会，2007年12月，東京

    

19. Development of Counter Rotating Axial Fan Turbojet Engine for Supersonic Unmanned Plane

    Minato, R., Ota, T., Fukutomi, K., Tanatsugu, N., Mizobata, K., Kojima, T., Kobayashi, H，Joint Propulsion Conference 2007，AIAA　Paper2007-5023巻，AIAA，2007年，Cinncinati

    

20. Development of Turbojet Engine for Supersonic Unmanned Plane

    Minato, R., Ota, T., Fukutomi, K., Tanatsugu, N., Mizobata, K., Kojima, T., Kobayashi, H.，2006 KSAS-JSASS Joint International Symposium on Aerospace Engineering.，日本航空宇宙学会，2006年，釜山

    

21. Preliminary Design of a Small Scaled Turbojet Engine for a Supersonic Flight Experimental Vehicle

    Ryojiro. Minato, Ikuo. Tokura, Nobuhiro. Tanatsugu, Takahiro. Himeno,，25 th International Symposium on Space Technologies and Science，ISTS　2006　g22巻，日本航空宇宙学会，2006年，金沢

    

22. Development of Turbojet Engine for Supersonic Unmanned Plane

    Minato. R，14th AIAA/AHI International Conference on Space Planes and Hypersonic Systems and Technologies, (2006)，AIAA 2006-8145巻，AIAA，2006年，キャンベラ

    

23. Development Study on a Small-scale Supersonic Flight Experiment Vehicle with Air-breathing Propulsion

    Mizobata, K., Minato. R, Kimura, H., Arai, T., Sugiyama, H., and Tanatsugu, N，13th AIAA/CIRA International Conference on Space Planes and Hypersonic Systems and Technologies，AIAA Paper 2005-3347巻，AIAA，2005年05月，Ｎａｐｌｅs

    

24. Preliminary Analysis of Turbojet Engine at Off-design Condition for Subscale Supersonic Unmanned Plane

    Minato, R., Arai, T., Himeno, T., Kobayashi, H., Mizobata, K. and Tanatsugu, N，13th AIAA/CIRA International Conference on Space Planes and Hypersonic Systems and Technologies，AIAA，2005年05月，Ｎａｐｌｅs

    

25. Numerical Analysis of Supersonic Combustion by a Plasma Torch

    Minato, R., Niioka, T., Sugiyama, H., Mizobata, K，13th AIAA/CIRA International Conference on Space Planes and Hypersonic Systems and Technologies，AIAA，2005年05月，Ｎａｐｌｅs

    

26. Correlation between Fluctuation of Mass Flux and Hydrogen Concentration in Supersonic Mixing,

    Arai, T., Mizobata, K., Minato, R., Tanatsugu, N, Mori, Y. and Kudo, T.，13th AIAA/CIRA International Conference on Space Planes and Hypersonic Systems and Technologies，AIAA Paper 2005-3236巻，AIAA，2005年05月，Ｎａｐｌｅs

    

27. Performance Analysis of Turbojet Engine with After Burner for Supersonic Unmanned Vehicle

    Kaneko, H., Minato, R., Arai, T., Himeno, T., Kobayashi, H., Mizobata, K., Tanatsugu, N，Asian Joint Conference of Propulsion And Power2005，日本航空宇宙学会，2005年01月，北九州

    

28. Off-design Analysis of Turbojet Engine for Supersonic Unmanned Plane", Asian Joint Conference on Propulsion and Power

    Minato, R., Arai, T., Himeno, T., Kobayashi, H., Mizobata, K., Tanatsugu, N.，Asian Joint Conference of Propulsion And Power，日本航空宇宙学会，2005年01月，北九州

    

29. Development Study at University Laboratories on a Small-scale Supersonic Flight Experiment Vehicle with Air-breathing Propulsion

    Mizobata, K., Minato. R, Arai, T., Sugiyama, H., and Tanatsugu, N，Mechanical Engineering Congress, 2004 Japan International Symposium “Space Development and Utilization Activities in University Laboratories，日本機械学会，2004年09月，札幌

    

30. Effect of Hydrogen Jet Position relative to Plasma Torch on Supersonic Combustion

    Minato, R., Niioka, N，12th AIAA International Conference on Space Planes and Hypersonic Systems and Technologies，AIAA 2003-6907巻，AIAA，2003年12月，Norfolk

    

31. Numerical Investigation of Hydrogen Combustion Using Plasma Torch in Supersonic Airflow

    Minato, R. and Niioka, T，Proceeding of The Third Asia-Pacific Conference on Combustion，(頁 726 ～ 729)，日本燃焼学会，2001年06月，ソウル