著書論文等- 永井 大樹 -
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件数:683件
[2008]
521.[] Enhancement of pressure-sensitive paint emission using localized surface plasmon resonance for shock tunnel applications.[46th AIAA Aerospace Sciences Meeting and Exhibit, (2008)]Y. Miura, H. Nagai, K. Asai, K. Nakakita
http://www.scopus.com/inward/record.url?eid=78149433077&partnerID=40
522.[] Surface pressure and flow field behind an oscillating fence submerged in turbulent boundary layer.[4th AIAA Flow Control Conference, (2008)]Manjinder S. Saini, Jonathan W. Naughton, Taro Yamashita, Hiroki Nagai, Keisuke Asai
http://www.scopus.com/inward/record.url?eid=78649290670&partnerID=40
523.[] *Study on Thermal Characteristics of A Small Loop Heat Pipe.[Journal of Thermal Science and Technology,3(2), (2008), 355-367-]Hosei Nagano, Hiroki Nagai, Fuyuko Fukuyoshi, Hiroyuki Ogawa
[2007]
524.[] 感圧・感温センシングのための色素連結型酸素透過性高分子の開発.[酸化反応討論会講演要旨集,40th, (2007), 149-151]小幡誠, 満尾和徳, 永井大樹, 浅井圭介, 矢野重信
525.[] 小型ループヒートパイプの研究(リザーバ制御による動作特性向上).[日本機械学会熱工学コンファレンス講演論文集,2007, (2007), 381-382]長野方星, 福吉芙由子, 小川博之, 永井大樹
526.[] Pressure-Sensitive Paint Measurement of the Flow around a Simplified Car Model.[Journal of Visualization,10(3),(2007),289-298]Yamashita,T., Sugiura, H., Nagai, H., Asai, K., Ishida, K.
527.[] Thermal Performance of a Miniature Loop Heat Pipe for spacecraft thermal control system.[2007 ASME-JSME Thermal Engineering Summer Heat Transfer Conference,(2007)]Nagai, H., Nagano, H., Fukuyoshi, F., Ogawa, H.
528.[] Measurement of Oxygen Partial Pressure Distribution in Fuel Cell using Pressure-Sensitive Paint.[2007 ASME-JSME Thermal Engineering Summer Heat Transfer Conference,(2007)]Inagaki, S., Nagai, H. , Asai, K.
529.[] 多孔質膜を用いた差圧応答型PSPの開発.[可視化情報学会誌,27(Suppl.1), (2007), 27-28]依田大輔, 永井大樹, 浅井圭介
10.3154/jvs.27.Supplement1_27
530.[] 感圧塗料による高速列車の後尾部流れの可視化.[可視化情報学会誌,27(Suppl.1), (2007), 13-16]小寺健幸, 山下太郎, 浅井圭介, 永井大樹, 森田潔
10.3154/jvs.27.Supplement1_13
531.[] Evaluation of Lifetime-based Pressure-Sensitive Paint Measurement in Low-speed Flow.[22nd International Congress on Instrumentation in Aerospace Simulation Facilities,(2007)]Yamashita, T.,Nagai, H.,Asai, K.
532.[] Development of Pressure-Sensitive Paint Technique in a Supersonic Blowdown Wind Tunnel and its Application to a Busemann Biplane.[22nd International Congress on Instrumentation in Aerospace Simulation Facilities,(2007)]Saito, K., Ogawa, T., Nagai, H., Asai, K.
533.[] 感温塗料を用いたエアロスパイクによる極超音速空力加熱の可視化実験.[衝撃波シンポジウム講演論文集,2006, (2007), 131-134]HA Seungwon, 石黒雄一, 三浦悠佑, 永井大樹, 浅井圭介, 中北和之
534.[] 極超音速空力加熱に対する衝撃波干渉の影響.[衝撃波シンポジウム講演論文集,2006, (2007), 121-124]石黒雄一, 三浦悠佑, 永井大樹, 浅井圭介, 中北和之
535.[] Visualization of Hypersonic Compression Corner Flows Using Temperature- and Pressure- Sensitive Paints.[45th AIAA Aerospace Science Meeting and Exhibit,(2007)]ISHIGURO, Y., OHMI, S., NAGAI, H., ASAI, K., NAKAKITA, K.
536.[] Unsteady Flow Measurements of a Slender Delta Wing in Wing Rock Motion.[45th AIAA Aerospace Science Meeting and Exhibit,(2007)]HIROSE, Y., NAGAI, H., KURASHINA, D., ASAI, K.
537.[] Nano-mega Scale Flow Dynamics for Advanced Aerospace.[Tohoku University Press,(2007)]Keisuke Asai, Hiroki Nagai
538.[] 機能性色素の合成と応用技術.[シーエムシー出版,(2007)]浅井圭介、永井大樹
539.[] MEMS/NEMS工学大全.[エヌティーエス株式会社,(2007)]浅井圭介、永井大樹
540.[] Pressure-sensitive paint measurement of the flow around a simplified car model.[Journal of Visualization,10(3),(2007),289-298]T. Yamashita, H. Sugiura, H. Nagai, K. Asai, K. Ishida
10.1007/BF03181696
http://www.scopus.com/inward/record.url?eid=38549091473&partnerID=40
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