論文- 永井 大樹 -
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件数:232件
[2013]
81.Non-Condensable Gas effect in Oscillating Heat Pipe.[Proceedings of 43rd International Conference on Environmental Systems,(2013)]Daimaru, T. and Nagai, H.
82.Numerical Simulation of Startup Behavior of Loop Heat Pipes with Secondary Wick.[Proceedings of 29th International Symposium on Space Technology and Science,(2013)]Magome, K., Taketani, M., Nagai, H.
83.Propeller Slipstream Interference with Wing Aerodynamic Characteristics of Mars Airplane at Low Reynolds Number.[Proceedings of 29th International Symposium on Space Technology and Science,(2013)]Makino, F., Nagai, H. and Asai, K.
84.Experimental Investigation of Non-condensable Gas effects on the Oscillating Heat Pipe.[Proceedings of 29th International Symposium on Space Technology and Science,(2013)]Daimaru, T. and Nagai, H.
85.Dynamic Behaviour of Mars Airplane with Folded-Wing Deployment.[Proceedings of 29th International Symposium on Space Technology and Science,(2013)]Fujita, K., Motoda, Y. and Nagai, H.
86.Characteristics of Low-Reynolds Number Airfoils in a Mars Wind Tunnel.[Proceedings of 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition,(2013)]Nagai, H., Asai, K., Numata, D., Suwa, T. and Anyoji, M.
87.Development of Ultrafast Response Anodized Aluminum Pressure-Sensitive Paints.[Proceedings of 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition,(2013)]Fujii, S., Numata, D., Nagai, H. and Asai, K.
88.火星探査飛行機用プロペラ開発のための翼型に関する研究.[日本航空宇宙学会論文集,61,(2013),421-]米 澤 宏 一,後 藤 雄 大,砂 田 茂,林 田 高 志,諏 訪 哲 也,酒 井 宣 明,永 井 大 樹,浅 井 圭 介,辻 本 良 信
89.Aerodynamic Characteristics and Effects of Winglets of the Boomless Tapered Supersonic Biplane during the Starting Process.[Trans. JSASS Aerospace Tech. Japan,11,(2013),17-26]Yamashita, H., Fujisono, T., Toyoda, A., Nagai, H., Asai, K., Jeong . and Obayashi, S.
90.Heat Transfer Performance of Oscillating Heat Pipe by Difference of Surface Characteristics.[Proceedings of the 17th International Heat Pipe Conference,(2013)]Hiroki Nagai, Takamu Kanayama, Takurou Daimaru
91.Experimental Study on Startup Behavior considering Gravity Effect of a Miniature Loop Heat Pipe.[Proceedings of the 17th International Heat Pipe Conference,(2013)]Hiroki Nagai, Horomichi Tamamura, Hosei Nagano, Hiroyuki Ogawa
[2012]
92.Conceptual Design with Aerial Deployment Mechanisms of Airplane for Mars.[Proceedings of 2012 Asia-Pacific International Symposium on Aerospace Technology,(2012)]Fujita, K., Nagai, H., Asai, K.
93.Heat Transfer Performance of Oscillating Heat Pipe by Difference of Surface Characteristics.[Proceedings of The 17th International Heat Pipe Conference,(2012)]Nagai, H., Kanayama, T., Daimaru, T.
94.Wind Tunnel Testing on Start/Unstart Characteristics of Finite Supersonic Biplane Wing.[AIAA Journal,(2012)]H. Yamashita, N. Kuratani, M. Yonezawa, T. Ogawa, H. Nagai, K. Asai and S. Obayashi,
95.Conceptual Design Method for a Mars Airplane: Formulation of Aerodynamic Characteristics at Low Reynolds Numbers.[Proceedings of the 9th International Conference on Flow Dynamics,(2012)]Fujita, K., Nagai, H., Asai, K.
96.Experiment verification of Acoustic Feedback Loop around NACA0012 Airfoil at Low Reynolds Number.[Proceedings of 9th International Conference Fluid Dynamics,(2012)]Sakai, N., Nagai, H., Asai, K., Ikeda, T. and Atobe, T.
97.Development of Ultrafast Time Response Pressure-Sensitive Paint for Visualization of Shock Wave Phenomena.[Proceedings of 9th International Conference Fluid Dynamics,(2012)]Fujii, S., Numata, D., Nagai, H. and Asai, K.
98.Transient Analysis of Loop Heat Pipes with Secondary Wick.[Proceedings of 9th International Conference Fluid Dynamics,(2012)]Magome, K., Taketani, M. and Nagai, H.
99.Non-Condensable Gas effect in Oscillating Heat Pipe.[Proceedings of 9th International Conference Fluid Dynamics,(2012)]Daimaru, T., Nagai, H.
100.Response Time Evaluation of Temperature-Sensitive Paint.[Proceedings of 9th International Conference Fluid Dynamics,(2012)]Horagiri, T., Nagai, H.
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