著書論文等- 永井 大樹 -
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件数:683件
[2015]
141.[] Development of Mars Exploration Aerial Vehicle in Japan.[Proceedings of the 30th International Symposium on Space Technology and Science,(2015)]Hiroki Nagai, Akira Oyama, Mars Airplane WG
142.[] A Parametric Study of Mars Airplane Concept for Science Mission on Mars.[Proceedings of the 30th International Symposium on Space Technology and Science,(2015)]Koji Fujita, Hiroki Nagai, Akira Oyama
143.[] Development of an Oscillating Heat Pipe Cooling System for GAPS.[Proceedings of the 30th International Symposium on Space Technology and Science,(2015)]Hideyuki Fuke, Takayoshi Inoue, Akiko Kawachi, Daisuke Matsumoto, Yoshiro Miyazaki, Hiroki Nagai Taku Nonomura, Hiroyuki Ogawa, Naoki Yamada, et al
144.[] Conceptual Design Study of Oscillating Heat Pipe System for GAPS.[Proceedings of the 30th International Symposium on Space Technology and Science,(2015)]Shun Okazaki, Hideyuki Fuke, Takayoshi Inoue, Akiko Kawachi, Daisuke Matsumoto, Yoshiro Miyazaki, Hiroki Nagai Taku Nonomura, Hiroyuki Ogawa, Naoki Yamada
145.[] Experimental Study in Effects of Secondary Wick Configuration on Thermal Performance of a Loop Heat Pipe.[Proceedings of the 30th International Symposium on Space Technology and Science,(2015)]Masahiko Taketani, Takuya Adachi, Hiroki Nagai
146.[] Pressure-sensitive paint technique for surface pressure measurements in a low-density wind tunnel.[Journal of Visualization,18(2),(2015),297-309]M. Anyoji, D. Numata, H. Nagai, K. Asai
10.1007/s12650-014-0239-9
http://www.scopus.com/inward/record.url?eid=84940007053&partnerID=40
147.[] Aerodynamic Evaluation of a Capsule Shaped Projectile during Free Flight Testing with Ballistic Range.[AIAA SciTech 2015,(2015)]Akiho Ishida, Hiroki Nagai, Hideyuki Tanno, Tomoyuki Komoro
148.[] Operational characteristics of the oscillating heat pipe with noncondensable gas.[Journal of Thermophysics and Heat Transfer,29(3),(2015),563-571]Takurou Daimaru, Hiroki Nagai
10.2514/1.T4461
http://gateway.isiknowledge.com/gateway/Gateway.cgi?&GWVersion=2&SrcAuth=TohokuUniv&SrcApp=TohokuUniv&DestLinkType=FullRecord&KeyUT=WOS:000357940400014&DestApp=WOS http://www.scopus.com/inward/record.url?eid=84940737228&partnerID=40
149.[] Operational Characteristics of the Oscillating Heat Pipe with Non-Condensable Gas.[Journal of Thermophysics and Heat Transfer,29(3),(2015),563-571]Daimaru, T., Nagai, H.
10.2514/1.T4461 2015
150.[] The applications of pressure-sensitive paint in microfluidic systems.[Microfluid Nanofluid,18(5),(2015),739-753]Chih-Yung Huang, Yu Matsuda, James W. Gregory, Hiroki Nagai, Keisuke Asai
151.[] Effects of Mach Number and Specific Heat Ratio on Low-Reynolds-Number Airfoil Flows.[AIAA Journal,53(6),(2015),1640-1654]Masayuki Anyoji, Daiju Numata, Hiroki Nagai, Keisuke Asai
152.[] Pressure-Sensitive Paint Technique for Surface Pressure Measurement in a Low Density Wind Tunnel.[Journal of Visualization,18(2),(2015),297-309]Masayuki Anyoji, Daiju Numata, Hiroki Nagai, Keisuke Asai
153.[] マルチエバポレータ型ループヒートパイプ内部流動特性に関する研究(微小重力下での蒸発器及び凝縮器の可視化).[日本機械学会論文集,81(827),(2015),15-00104-]松田雄太,長野方星,岡崎峻,小川博之,永井大樹
1299/transjsme.15-00104, 2015
154.[] マルチエバポレータ型ループヒートパイプの内部流動特性に関する研究(微小重力環境下での蒸発器及び凝縮器の可視化).[日本機械学会論文集,81(827),(2015),15-00104-15-00104]松田 雄太, 長野 方星, 岡崎 峻, 小川 博之, 永井 大樹
10.1299/transjsme.15-00104
155.[] Aerodynamic evaluation of a capsule shaped projectile during free flight testing with ballistic range.[53rd AIAA Aerospace Sciences Meeting, (2015)]Akiho Ishida, Hiroki Nagai, Hideyuki Tanno, Tomoyuki Komuro
10.2514/6.2015-0244
http://www.scopus.com/inward/record.url?eid=84980347780&partnerID=40
156.[] 先進熱制御デバイスを用いたDESTINY熱設計.[宇宙科学技術連合講演会講演集(CD-ROM),59th, (2015), ROMBUNNO.2G06-]岡崎峻, 長野方星, 永井大樹, 小川博之, 川勝康弘
157.[] 自励振動ヒートパイプの動作特性における逆止弁の影響.[宇宙科学技術連合講演会講演集(CD-ROM),59th, (2015), ROMBUNNO.3M12-]大丸拓郎, 吉田周平, 永井大樹, 岡本篤, 安藤麻紀子, 田中洸輔, 杉田寛之
158.[] Loop Heat Pipeの熱輸送向上を目指したセカンダリウィック最適形状の提案.[宇宙科学技術連合講演会講演集(CD-ROM),59th, (2015), ROMBUNNO.3M14-]安達拓矢, 竹谷雅彦, 大丸拓郎, 永井大樹
159.[] 火星飛行機の空中展開に対するヒンジ軸傾斜の効果.[宇宙科学技術連合講演会講演集(CD-ROM),59th, (2015), ROMBUNNO.1E07-]藤田昂志, 永井大樹, 大山聖
160.[] マルチエバポレータ型ループヒートパイプの内部可視化に基づく熱流動モデルの提案.[宇宙科学技術連合講演会講演集(CD-ROM),59th, (2015), ROMBUNNO.3M15-]木澤雅文, 長野方星, 岡崎峻, 小川博之, 永井大樹
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