著書論文等- 永井 大樹 -
表示方法: 表示形式: 表示順:
[]:著書 []:論文 []:総説・解説記事
件数:683件
[2014]
181.[] 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
182.[] 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
183.[] 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
184.[] 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.
185.[] 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.
186.[] 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
187.[] Numerical Analysis for an Aerial Deployment Motion of a Folded-Wing Airplane.[Proceedings of AIAA SciTech2014,(2014)]Fujita, K., Motoda, T. and Nagai, H.
188.[] Development of Temperature-Sensitive Paint with High Performance and Responsivity for Aerodynamic Heating Measurement.[Proceedings of AIAA SciTech2014,(2014)]Horagiri, T. and Nagai, H.
189.[] Propeller Slipstream Interference with Wing Aerodynamic Characteristics of Mars Airplane at Low Reynolds Number.[Proceedings of AIAA SciTech2014,(2014)]Makino, F. and Nagai, H.
190.[] 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
191.[] 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
192.[] 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
193.[] 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
194.[] 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.
195.[] 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
196.[] 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
197.[] 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
198.[] PSPの低速流れへの応用.[可視化情報学会誌,34(132), (2014), 16-21]依田大輔,浅井圭介,永井大樹,沼田大樹
199.[] 次世代高温環境センサの展望と産業応用.[非破壊検査,63(12), (2014), 1-8]高木敏行,庄司一夫,和佐泰宏,米津豊作,冨田健夫,風岡学,永井大樹, 町島祐一,内一哲哉
200.[] 第46回流体力学講演会/第32回航空宇宙数値シミュレーション技術シンポジウム開催報告(トピックス).[日本航空宇宙学会誌,62(11), (2014), 380-381]永井 大樹
10.14822/kjsass.62.11_380
Page: [prev] [1] [2] [3] [4] [5] [6] [7] [8] [9] [10] [11] [12] [13] [14] [15] [16] [17] [18] [19] [20] [21] [22] [23] [24] [25] [26] [27] [28] [29] [30] [31] [32] [33] [34] [35] [next]
戻るこのページのトップへ
copyright(c)2005 Tohoku University