論文- 永井 大樹 -
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件数:235件
[2014]
61.Propeller Slipstream Interference with Wing Aerodynamic Characteristics of Mars Airplane at Low Reynolds Number.[Proceedings of AIAA SciTech2014,(2014)]Makino, F. and Nagai, H.
62.Numerical Analysis for an Aerial Deployment Motion of a Folded-Wing Airplane.[Proceedings of AIAA SciTech2014,(2014)]Fujita, K., Motoda, T. and Nagai, H.
63.自励振動ヒートパイプにおける非凝縮ガスの影響.[航空宇宙技術,13,(2014),17-24]大丸拓郎,永井大樹
64.Effects of Mach Number and Specific Heat Ratio on Airfoils at Low Reynolds Numbers.[AIAA Journal,(2014)]Anyoji, M., Numata, D., Nagai, H. and Asai, K.
65.Control Surface Effectiveness of Low Reynolds Number Flight Vehicles.[Journal of Fluid Science and Technology,9(5),(2014),14-00176-]M. Anyoji, M. Okamoto, H. Hidaka, K. Kondo, A. Oyama, H. Nagai, K. Fujii
66.Computational and Experimental Analysis of a High Performance Airfoil under Low-Reynolds Number Flow Condition.[Journal of Aircraft,(2014)]M. Anyoji, T. Nonomura, H. Aono, A. Oyama, K. Fujii, H. Nagai, K. Asai,
10.2514/I.C032553
67.Operating characteristics of multiple evaporators and multiple condensers loop heat pipe with polytetrafluoroethylene wicks.[Journal of Electric Cooling and Thermal Control,4(1),(2014),22-32]Shou Okutani, Hosei Nagano, Shun Okazaki, Hiroyuki Ogawa and Hiroki Nagai
68.Operation Characteristics of Loop Heat Pipes with PTEF and SUS wicks.[Proceedings of the 44th International Conference on Environmental Systems,(2014)]Shun Okazaki, Hiroyuki Ogawa, Hosei Nagano, Hiroki Nagai
69.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,62(1),(2014),24-30]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
10.2322/jjsass.62.24
[2013]
70.Aerial-Wing-Deployment Simulation of the Folded-Wing Airplane with Individual Aerodynamic Characteristics.[Proceedings of The 2013 Asia-Pacific International Symposium on Aerospace Technology,(2013)]Fujita, K., Motoda, T. and Nagai, H.
71.Mission Scenario of Mars Exploration by Airplane.[Proceedings of The 2013 Asia-Pacific International Symposium on Aerospace Technology,(2013)]Nagai, H. and Oyama, A.
72.Development of High-Performance TSP by Mixing Fine Particle.[Proceedings of 10th International Conference on Fluid Dynamics,(2013),698-699]Horagiri, T., Nagai, H.
73.Flow-Coupled Multibody Dynamics Simulation for an Aerial Deployment of a Folded Wing.[Proceedings of 10th International Conference on Fluid Dynamics,(2013),726-727]Fujita, K., Motoda, T. and Nagai, H.
74.Aerodynamic Influence of a Propeller Wake on NACA0012 Airfoil at Low Reynolds Number.[Proceedings of 10th International Conference on Fluid Dynamics,(2013),650-651]Makino. F., Nagai, H.
75.Effect of Secondary Wick on Startup Process of Loop Heat Pipe.[Proceedings of 10th International Conference on Fluid Dynamics,(2013),696-697]Taketani. M., Nagai, H.
76.Development of Phosphor-TSP for High-Temperature Distribution Measurement.[Proceedings of 10th International Conference on Fluid Dynamics,(2013),740-741]Ishida, A., Nagai, H.
77.Experimental Study on Startup Behavior considering Gravity Effect of a Miniature Loop Heat Pipe.[Proceedings of The 17th International Heat Pipe Conference,(2013)]Nagai, H., Tamamura, H., Nagano, H., Ogawa. H.
78.Preliminary design and thermal analysis of a miniature Mars airplane thermal control system.[Proceedings of 43rd International Conference on Environmental Systems,(2013)]Daimaru, T. and Nagai, H.
79.Numerical Study on Shock Wave Interaction over Compression Corner with 30 deg. in Hypersonic Flow.[Proceedings of 29th International Symposium on Shock Waves,(2013)]Kuramoto, T., Tsuboi, N. and Nagai, H., Asai, K.
80.Operational characteristics of the Oscillating Heat Pipe with non-condensable gas.[Proceedings of 43rd International Conference on Environmental Systems,(2013)]Daimaru, T. and Nagai, H.
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