Fujii Kozo | Institute of Space and Astronautical Science (ISAS)
スポンサーリンク
概要
関連著者
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Fujii Kozo
Institute of Space and Astronautical Science (ISAS)
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FUKUDA Kota
School of Engineering, Department of Aeronautics and Astronautics, Tokai University
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ISHII Tatsuya
Aerospace Research and Development Directorate (ARD), Japan Aerospace Exploration Agency (JAXA)
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Teramoto Susumu
University Of Tokyo Department Of Aeronautics And Astronautics
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Fujii K
Institute Of Space And Astronautical Science (isas)
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Hiraki Kouju
Institute of Space and Astronautical Science (ISAS)
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Hiraki K
Institute Of Space And Astronautical Science (isas)
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Fujii Kozo
Institute Of Space And Astronautical Science Japan Aerospace Exploration Agency
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Kawai Soshi
Postdocrtal research fellow, Dept. of Aeronautics and Astronautics, The University of Tokyo
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Kawai Soshi
Postdocrtal Research Fellow Dept. Of Aeronautics And Astronautics The University Of Tokyo
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TSUTSUMI Seiji
JAXA’s Engineering Digital Innovation (JEDI) Center, Japan Aerospace Exploration Agency (JAXA)
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UI Kyoichi
Space Transportation Mission Directorate/Epsilon Rocket Project Team, Japan Aerospace Exploration Ag
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TAKAKI Ryoji
JAXA’s Engineering Digital Innovation (JEDI) Center, Japan Aerospace Exploration Agency (JAXA)
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Fujii Kozo
Institute Of Space And Astronautical Science (isas) Japan Aerospace Exploration Agency (jaxa)
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Ui Kyoichi
Space Transportation Mission Directorate/epsilon Rocket Project Team Japan Aerospace Exploration Agency (jaxa)
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Fukuda Kota
School Of Engineering Department Of Aeronautics And Astronautics Tokai University
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Ishii Tatsuya
Aerospace Research And Development Directorate (ard) Japan Aerospace Exploration Agency (jaxa)
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Tsutsumi Seiji
Jaxa's Engineering Digital Innovation (jedi) Center Japan Aerospace Exploration Agency (jaxa)
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Takaki Ryoji
Jaxa's Engineering Digital Innovation (jedi) Center Japan Aerospace Exploration Agency (jaxa)
著作論文
- Numerical Analysis of Dynamic Instability at Transonic Speeds
- An Acoustic Impedance Model for Evaluating the Ground Effect of Static-Firing Tests on a Rocket Motor
- W02-1-(2) Some Remarks on the LES/RANS Hybrid Methods for Compressible Flow Simulations(International Minisymposium on Challenger and Advances in Flow Simulation and Modeling,Mechanical Engineering Congress, 2005 Japan (MECJ-05))
- An Acoustic Impedance Model for Evaluating the Ground Effect of Static-Firing Tests on a Rocket Motor