学会等発表 - 湊　亮二郎

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

    Ryojiro Minato，Joint Propulsion Conference 2007，American Institute of Aeronautics and Astronautics，2007年07月，Cincinnati，アメリカ合衆国

42. Development of Turbojet Engine for Supersonic Unmanned Plane

    Ryojiro Minato，14th AIAA/AHI International Conference on Space Planes and Hypersonic Systems and Technologies，American Institute of Aeronautics and Astronautics，AIAA Paper 2006-8145，2006年11月，Canberra，オーストラリア連邦

43. Development of Turbojet Engine for Supersonic Unmanned Plane

    Ryojiro Minato，2006 KSAS-JSASS Joint International Symposium on Aerospace Engineering，Japanese Society of Aeronautics and Space Science，2006年11月，釜山，大韓民国

44. reliminary Design of a Small-Scale Turbojet Engine for a Supersonic Flight Experimental Vehcle

    Ryojiro Minato，25th International Symposium on Space Techmology and Science，Japanese Society of Aeronautics and Space Science，2006年06月，金沢，日本国

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

    Kazuhide Mizobata，13th International Space Planes and Hypersonic Systems and Technologies Conference，American Institute of Aeronautics and Astronautics，AIAA Paper 2005-3347，2005年05月，Naples，イタリア共和国

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

    Arai，13th International Space Planes and Hypersonic Systems and Technologies Conference，American Institute of Aeronautics and Astronautics，AIAA Paper 2005-3236，2005年05月，Naples，イタリア共和国

47. Numerical Analysis of Supersonic Combustion by a Plasma Torch

    Minato, R., Niioka, T., Sugiyama, H. and Mizobata, K，13th International Space Planes and Hypersonic Systems and Technologies Conference，American Institute of Aeronautics and Astronautics，AIAA Paper 2005-3424，2005年05月，Naples, Italy，イタリア共和国

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

    Arai，13th International Space Planes and Hypersonic Systems and Technologies Conference，American Institute of Aeronautics and Astronautics，AIAA Paper 2005-3236，2005年05月，Italy

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

    Ryojiro Minato, Takakage, Arai, Takehiro Himeno,Hiroaki Kobayashi, Kazuhide Mizobata, Nobuhiro Tanatsugu，Asian Joint Conference on Propulsion And Power，Japanese Society of Aeronautics and Space Science，2005年01月27日，Kitakyushu, Japan，日本国

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

    Hiroki Kaneko, Ryojiro Minato, Takakage, Arai, Takehiro Himeno,Hiroaki Kobayashi, Kazuhide Mizobata, Nobuhiro Tanatsugu，Asian Joint Conference on Propulsion And Power，Japanese Society of Aeronautics and Space Science，2005年01月27日，Kitakyushu，日本国

51. 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，日本機会学会，2004年09月，札幌，日本国

52. Effects of Hydrogen Jet Position relative to Plasma Torch on Supersonic Combustion

    湊　亮二郎，12th International Space Planes and Hypersonic Systems and Technologies Conference，American Institute of Aeronautics and Astronautics，AIAA Paper2003-6908，2003年12月15日，Norflok, Virginia, USA，アメリカ合衆国

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

    湊　亮二郎，The 3rd Asia-Pacific Conference on Combustion，Korean Society of Combustion，Proceedings of The 3rd Asia-Pacific Conference on Combustion，2001年06月24日，Seoul, Korea，大韓民国