Presentaion at conference, meeting, etc. - Minato Ryojiro
-
Development of Counter Rotating Axial Fan Turbojet Engine for Supersonic Unmanned Plane
Ryojiro Minato,Joint Propulsion Conference 2007,American Institute of Aeronautics and Astronautics,2007.07,Cincinnati,United States
-
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 2006-8145,2006.11,Canberra,Australia
-
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,2006.11,釜山,Korea, Republic of
-
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,2006.06,金沢,Japan
-
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 2005-3347,2005.05,Naples,Italy
-
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 2005-3236,2005.05,Naples,Italy
-
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 2005-3424,2005.05,Naples, Italy,Italy
-
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 2005-3236,2005.05,Italy
-
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,2005.01.27,Kitakyushu, Japan,Japan
-
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,2005.01.27,Kitakyushu,Japan
-
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,2004.09,札幌,Japan
-
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 Paper2003-6908,2003.12.15,Norflok, Virginia, USA,United States
-
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,2001.06.24,Seoul, Korea,Korea, Republic of