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件数:694件
[2015]
141.[] 可視化によるチェックバルブ付き自励振動ヒートパイプの循環流に関する考察.[Thermophysical Properties,36th, (2015), 84‐86-]吉田周平, 大丸拓郎, 永井大樹, LIU Tianshu, 沼田大樹, 浅井圭介
142.[] 逆止弁付き振動流型ヒートパイプの設計最適化を目指した熱輸送特性評価.[Thermophysical Properties,36th, (2015), 66‐68-]田中洸輔, 安藤麻紀子, 岡本篤, 杉田寛之, 大丸拓郎, 永井大樹
143.[] 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.[日本機械学会年次大会講演論文集(CD-ROM),2015, (2015), ROMBUNNO.S1910301-]長山剛大, 永井大樹, 丹野英幸, 小室智幸
144.[] Visualization of Loop Heat Pipe with Multiple Evaporators under Microgravity.[Proceedings of the 45th International Conference on Environmental Systems,(2015)]Hosei Nagano, Yuta Matsuda, Shun Okazaki, Hiroki Nagai, Hiroyuki Ogawa
145.[] Parametric Study of Oscillating Heat Pipes by using Mathematical Model for Practical Use in Spacecraft.[Proceedings of the 30th International Symposium on Space Technology and Science,(2015)]Takurou Daimaru, Shuhei Yoshida, Hiroki Nagai, Atsushi Okamoto, Makiko Ando, Hiroyuki Sugita
146.[] Aerodynamic Characteristics of Airfoils with Different Aspect Ratio behind Propeller Slipstream in Low Reynolds Number Condition.[Proceedings of the 30th International Symposium on Space Technology and Science,(2015)]Hiroki Nagai, Kotaro Watanabe, Koji Fujita
147.[] Aerodynamic Challenge to Realize Mars Airplane.[Proceedings of the 30th International Symposium on Space Technology and Science,(2015)]Hiroki Nagai, Masayuki Anyoji, Taku Nonomura, Akira Oyama, Masato Okamoto, Gaku Sasaki, Takaaki Matsumoto, Kouichi Yonemoto, Kasahiro Kanazaki, Shigeru Sunada, Koichi Yonezawa, Masaru Koike, Koji Fujita, Keisuke Asai, Kozo Fujii
148.[] 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
149.[] 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
150.[] 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
151.[] 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
152.[] 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
153.[] 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
154.[] 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
155.[] 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
156.[] 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
157.[] 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
158.[] 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
159.[] 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
160.[] 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
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