著書論文等- 永井 大樹 -
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件数:694件
[2007]
561.[] 小型ループヒートパイプの伝熱流動特性(第一報 起動特性および熱輸送特性評価).[宇宙科学技術連合講演会講演集(CD-ROM),51st, (2007), 3J15-]福吉芙由子, 長野方星, 小川博之, 永井大樹
562.[] A102 寿命法による感圧塗料計測の低速流への適用と評価.[可視化情報学会誌,27(1), (2007), 17-18]山下 太郎, 永井 大樹, 浅井 圭介
10.3154/jvs.27.Supplement1_17
563.[] Unsteady flow measurements of a slender delta wing in wing rock motion.[Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting,2, (2007), 1401-1412]Yuichi Hirose, Hiroki Nagai, Keisuke Asai
http://www.scopus.com/inward/record.url?eid=34250893923&partnerID=40
564.[] Visualization of hypersonic compression corner flows using temperature- And pressure-sensitive paints.[Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting,2, (2007), 1331-1342]Y. Ishiguro, H. Nagai, K. Asai, K. Nakakita
http://www.scopus.com/inward/record.url?eid=34250816391&partnerID=40
[2006]
565.[] Molecular Sensors in Microturbine Measurement.[Proceedings of 2006 ASME International Mechanical Engineering Congress and Exposition,(2006)]HUANG, C.Y., Gregory, J. W., NAGAI, H., ASAI,K., Sullivan, J. P.
566.[] Application of Luminophore-Pendant Pressure-Sensitive Paint to Fluid Dynamic Measurements.[Proceedings of 12th International Symposium on Flow Visualization,(2006)]SAKAUE, H., MITSUO, K., IIJIMA, Y., MORITA, K., HYAKUTAKE, T., TAGUCHI, H., NISHIDE, H., KOJIMA, T., NAGAI, H., ASAI, K.
567.[] Flow Diagnostic using PSP and TSP technique in a Supersonic Micronozzle.[Proceedings of 12th International Symposium on Flow Visualization,(2006)]NAGAI, H., NARAOKA, R., SAWADA, K., ASAI, K.
568.[] PSP Measurement of the Flow around a Simplified Car Model.[Proceedings of 12th International Symposium on Flow Visualization,(2006)]Yamashita,T., Sugiura, H., Nagai, H., Asai, K., Ishida, K.
569.[] 極超音速空力加熱率計測におけるTSP皮膜の影響.[可視化情報学会誌,26(Suppl.1), (2006), 201-204]永井大樹, 近江俊輔, 浅井圭介, 中北和之
10.3154/jvs.26.Supplement1_201
570.[] 感温塗料を用いた衝撃波干渉による三次元渦構造の可視化.[衝撃波シンポジウム講演論文集,2005, (2006), 79-82]石黒雄一, 近江俊輔, 永井大樹, 浅井圭介, 中北和之
571.[] ブラスト波が誘起する非定常圧力場の画像計測に関する研究.[衝撃波シンポジウム講演論文集,2005, (2006), 71-72]三浦悠佑, 石黒雄一, 永井大樹, 浅井圭介, 佐宗章弘
572.[] Cryogenic infrared mission "jAXA/SPICA" with advanced cryocoolers.[Cryogenics,46(2-3), (2006), 149-157]Hiroyuki Sugita, Takao Nakagawa, Hiroshi Murakami, Atsushi Okamoto, Hiroki Nagai, Masahide Murakami, Katsuhiro Narasaki, Masayuki Hirabayashi
10.1016/j.cryogenics.2005.11.017
http://www.scopus.com/inward/record.url?eid=33244482892&partnerID=40
573.[] PSP measurement of Pressure Distribution in a Supersonic Micronozzle.[44th AIAA Aerospace Science Meeting and Exhibit,(2006)]NAGAI, H., NARAOKA, R., SAWADA, K., ASAI, K.
574.[] Application of Lifetime Imaging Method to a Cryogenic Wind Tunnel.[44th AIAA Aerospace Science Meeting and Exhibit,(2006)]KOJIMA, T., NAGAI, H., ASAI, K., MITSUO, K., IIJIMA, Y., SAKAUE, H.
575.[] Effect of TSP Layer Thickness on Global Heat Transfer Measurement in Hypersonic Flow.[44th AIAA Aerospace Science Meeting and Exhibit,(2006)]OHMI, S., NAGAI, H., ASAI, K., NAKAKITA, K.
576.[] Cryogenic Infrared Mission “JAXA/SPICA” with Advanced Cryocoolers.[Cryogenics,(2006)]H.Sugita, T. Nakagawa, H. Murakami, A. Okamoto, H. Nagai, M. Murakami, K. Narasaki, M. Hirabayashi, SPICA Working Group
577.[] PSP measurement of pressure distribution in a supersonic micronozzle.[Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting,17, (2006), 12552-12561]H. Nagai, R. Naraoka, K. Sawada, K. Asai
http://www.scopus.com/inward/record.url?eid=34250854634&partnerID=40
578.[] C209 極超音速空力加熱率計測におけるTSP皮膜の影響.[可視化情報学会誌,26(1), (2006), 201-204]永井 大樹, 近江 俊輔, 浅井 圭介, 中北 和之
579.[] G303 感圧塗料を用いた単純自動車模型まわりの流れ場計測(2)(GS-3 流体計測,一般セッション).[流体工学部門講演会講演論文集,2006(0), (2006), _G303-1_-_G303-4_]杉浦 光, 山下 太郎, 永井 大樹, 浅井 圭介, 石田 圭太郎
10.1299/jsmefed.2006._G303-1_
580.[] G303 感圧塗料を用いた単純自動車まわりの流れ場計測(1)(GS-3 流体計測,一般セッション).[流体工学部門講演会講演論文集,2006(0), (2006), _G303-a_]杉浦 光, 山下 太郎, 永井 大樹, 浅井 圭介, 石田 圭太郎
10.1299/jsmefed.2006._G303-a_
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