Aoyama Takashi | Japan Aerospace Exploration Agency
スポンサーリンク
概要
関連著者
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Aoyama Takashi
Japan Aerospace Exploration Agency
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YANG Choongmo
Japan Aerospace Exploration Agency (JAXA)
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Yang Choongmo
Japan Aerospace Exploration Agency
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Aoyama T
Japan Aerospace Exploration Agency
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KONDO Natsuki
Japan Aerospace Exploration Agency
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Saito S
Japan Aerospace Exploration Agency
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Aoyama Takashi
Japan Aerospace Exploration Agency (jaxa)
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SAITO Shigeru
Japan Aerospace Exploration Agency
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JEONG Shinkyu
Institute of Fluid Science, Tohoku University
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Jeong Shinkyu
Institute Of Fluid Science Tohoku University
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INADA Yoshinobu
Japan Aerospace Exploration Agency (JAXA)
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SASAKI Toru
Institute of Molecular and Cellular Biosciences, University of Tokyo
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Kondo Natsuki
航空宇宙技術研究所
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Yee Kwanjung
Department Of Aerospace Engineering Pusan National University
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Sato Tetsuya
School Of Fundamental Science And Engineering Waseda University
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CHAE Sanghyun
Department of Aerospace Engineering, Pusan National University
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Chae Sanghyun
Department Of Aerospace Engineering Pusan National University
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Hashimoto Atsushi
Japan Aerospace Exploration Agency
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NAMBU Taisuke
Graduate School of Fundamental Science and Engineering, Waseda University
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Nambu Taisuke
Graduate School Of Fundamental Science And Engineering Waseda University
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Sasaki Toru
Institute Of Fluid Science Tohoku University
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Moriyama Takashi
Chiba University
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Liu Hao
Chiba University
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Maeda Masateru
Chiba University
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Aono Hikaru
University of Michigan
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SASAKI Toru
Institute of Applied Microbiology, The University of Tokyo
著作論文
- Aerodynamic Analysis of Helicopter Rotor by Coupling of CFD and Trim Calculation(Proceedings of the 15th NAL Symposium on Aircraft Computational Aerodynamics)
- Aerodynamic/Acoustic Analysis for Main Rotor and Tail Rotor of Helicopter
- Numerical Analysis of Sound Generation and Transmission from Flapping Wings
- Numerical Analysis of Maneuvering Rotorcraft Using Moving Overlapped Grid Method
- Design Exploration of Helicopter Blades for HSI Noise and Aerodynamic Performance
- Numerical Analysis of Flow through a Hole for Modeling of Wind Tunnel Porous Wall