著書論文等- 永井 大樹 -
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件数:683件
[2015]
161.[] 低レイノルズ数におけるプロペラ後流の影響を受けた三次元翼空力特性.[流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム講演集(CD-ROM),47th-33rd, (2015), ROMBUNNO.2D08-]永井大樹, 渡辺高太郎
162.[] S1910301 感温塗料を用いた高温衝撃風洞におけるHIFiRE模型の境界層遷移可視化.[年次大会,2015(0), (2015), _S1910301--_S1910301-]長山 剛大, 永井 大樹, 丹野 英幸, 小室 智幸
10.1299/jsmemecj.2015._S1910301-
[2014]
163.[] 高温環境における非破壊検査の現状と展望 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), 604-611]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
164.[] Computational and experimental analysis of a high-performance airfoil under low-reynolds-number flow condition.[Journal of Aircraft,51(6),(2014),1864-1872]Masayuki Anyoji, Taku Nonomura, Hikaru Aono, Akira Oyama, Kozo Fujii, Hiroki Nagai, Keisuke Asai
10.2514/1.C032553
http://gateway.isiknowledge.com/gateway/Gateway.cgi?&GWVersion=2&SrcAuth=TohokuUniv&SrcApp=TohokuUniv&DestLinkType=FullRecord&KeyUT=WOS:000345980800015&DestApp=WOS http://www.scopus.com/inward/record.url?eid=84914171144&partnerID=40
165.[] 火星探査航空機WGにおける空力研究のこれまでの成果と現状.[宇宙科学技術連合講演会講演集,58, (2014), 6p-]永井 大樹, 安養寺 正之, 野々村 拓
166.[] セカンダリウィックの形状がループヒートパイプの動作に与える影響.[宇宙科学技術連合講演会講演集,58, (2014), 6p-]竹谷 政彦, 永井 大樹
167.[] 自励振動ヒートパイプのスタートアップに関する一考察.[宇宙科学技術連合講演会講演集,58, (2014), 5p-]大丸 拓郎, 吉田 周平, 永井 大樹
168.[] DESTINY応用 : 火星気象衛星と火星航空機によるダスト輸送メカニズムの解明ミッション.[宇宙科学技術連合講演会講演集,58, (2014), 4p-]小郷原 一智, 大山 聖, 永井 大樹
169.[] 火星着陸探査技術実証機への搭載を目指した火星飛行機の概念設計.[宇宙科学技術連合講演会講演集,58, (2014), 6p-]藤田 昂志, 永井 大樹, 大山 聖
170.[] Visualization of Laminar to Turbulent Transition on Re-entry Capsule using TSP in High Enthalpy Shock Tunnel.[Proceedings of the 11th International Conference on Flow Dynamics,(2014)]Takehiro Nagayama, Takehito Horagiri, Hiroki Nagai, Hideyuki Tanno, Tomoyuki Komuro
171.[] Aerodynamic performance of optimized airfoil for Mars Airplane using Multi-objective generic algorithm.[Proceedings of the 11th International Conference on Flow Dynamics,(2014)]Kentaro Yamahara, Hiroki Nagai, Takaya Sato and Masahiro Kanazaki
172.[] Effect of blade wake by means of interference with propeller slipstream on low Reynolds number condition.[Proceedings of the 11th International Conference on Flow Dynamics,(2014)]Satoru Hattori, Kotaro Watanabe, Hiroki Nagai
173.[] Improvement of Startup Characteristics of a Loop Heat Pipe using Secondary Wicks.[Proceedings of the 11th International Conference on Flow Dynamics,(2014)]Masahiko Taketani, Hiroki Nagai
174.[] 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
175.[] 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
176.[] 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
177.[] 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
178.[] 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
179.[] 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
180.[] 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
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