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件数:694件
[2014]
181.[] Study of Motion Modeling for a Capsule Shaped Projectile in Free flight Testing at Transonic.[Proceedings of the 11th International Conference on Flow Dynamics,(2014)]Akiho Ishida, Hiroki Nagai, Hideyuki Tanno, Tomoyuki Komoro
182.[] Numerical Investigation of the Effects of Initial Liquid-Vapor Distribution in Oscillating Heat Pipes.[Proceedings of the 11th International Conference on Flow Dynamics,(2014)]Takurou Daimaru, Shuhei Yoshida, Hiroki Nagai, Atsushi Okamoto, Makiko Ando, Hiroyuki Sugita
183.[] LPSO型Mg合金を用いた火星探査航空機用軽量翼構造の試作.[日本学術会議材料工学連合講演会講演論文集,58th, (2014), 122-123]竹内伸介, 佐藤英一, 大山聖, 永井大樹
184.[] Numerical Study of Wind-Tunnel Acoustic Resonance induced by Two-Dimensional Airfoil Flow at Low Reynolds Number.[Proceedings of the 29th Congress of the International Council of the Aeronautical Science,(2014)]1. Tomoaki Ikeda, Takashi Atobe, Yasuhiro Konishi, Hiroki Nagai, Keisuke Asai
185.[] カプセル形状模型の自由飛行計測における空力特性評価.[日本機械学会年次大会講演論文集(CD-ROM),2014, (2014), ROMBUNNO.S1910203-]石田照歩, 永井大樹, 丹野英幸, 小室智幸
186.[] Mathematical Modeling and Experimental Validation of Oscillating Heat Pipes.[Proceedings of 44rd International Conference on Environmental Systems,(2014)]Takurou Daimaru, Shuhei Yoshida, Hiroki Nagai, Atsushi Okamoto, Makiko Ando and Hiroyuki Sugita
187.[] Effects of Secondary Wicks on the Thermal Performance of a Loop Heat Pipe.[Proceedings of 44rd International Conference on Environmental Systems,(2014)]Masahiko Taketani and Hiroki Nagai
188.[] Operation Characteristics of Loop Heat Pipes with PTEF and SUS wicks.[Proceedings of 44rd International Conference on Environmental Systems,(2014)]Shun Okazaki, Hosei Nagano, Hiroki Nagai and Hiroyuki Ogawa
189.[] Visualization of a Re-entry Vehicle in Hypersonic Flow using Temperature-Sensitive Paint.[Proceedings of the 16th International Symposium on Flow Visualization,(2014)]Hiroki Nagai, Takehito Horagiri, Hideyuki Tannno and Tomoyuki Komuro
190.[] Dynamic Behaviour of Mars Airplane with Folded-Wing Deployment.[Trans. of JSASS Aerospace Tech. Japan,12(ists29),(2014),Pk_1-Pk_6]Fujita, K, Motoda, T. and Nagai, H.
191.[] Wind Tunnel Testing on Start/Unstart Characteristics of Finite Supersonic Biplane Wing.[International Journal of Aerospace Engineering,2013,(2014)]Hiroshi Yamashita, Naoshi Kuratani, Masahito Yonezawa, Toshihiro Ogawa, Hiroki Nagai, Keisuke Asai and Shigeru Obayashi
10.1155/2013/231434
192.[] Propeller Slipstream Interference with Wing Aerodynamic Characteristics of Mars Airplane at Low Reynolds Number.[Trans. of JSASS Aerospace Tech. Japan,12(ists29),(2014),Tk_13-Tk_18]Making, F. and Nagai, H.
193.[] Development of Temperature-Sensitive Paint with High Performance and Responsivity for Aerodynamic Heating Measurement.[Proceedings of AIAA SciTech2014,(2014)]Horagiri, T. and Nagai, H.
194.[] Propeller Slipstream Interference with Wing Aerodynamic Characteristics of Mars Airplane at Low Reynolds Number.[Proceedings of AIAA SciTech2014,(2014)]Makino, F. and Nagai, H.
195.[] Numerical Analysis for an Aerial Deployment Motion of a Folded-Wing Airplane.[Proceedings of AIAA SciTech2014,(2014)]Fujita, K., Motoda, T. and Nagai, H.
196.[] 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
197.[] PSPの低速流れへの応用.[可視化情報学会誌,34(132), (2014), 16-21,1(2)-]依田大輔, 浅井圭介, 永井大樹, 沼田大樹
198.[] 未利用熱エネルギー活用の新開発と【採算性を重視した】熱省エネ新素材・新製品設計/採用のポイント.[株式会社 技術情報協会,(2014)]永井大樹
199.[] 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.
200.[] 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
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