著書論文等- 永井 大樹 -
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件数:694件
[2010]
401.[] Experimental Study on Dynamic Instability of Re- Entry Capsule-Shaped Body using Pressure- Sensitive Paint.[48th AIAA Aerospace Science Meeting and Exhibit,(2010)]SUGIMOTO, D., NAGAI, H., ASAI, K., HIRAKI, K.
402.[] Experimental Study of Heat Transfer Measurement using Temperature-Sensitive Paint for High-Temperature Application in Hypersonic Flow.[49th AIAA Aerospace Science Meeting and Exhibit,(2010)]Hiroki Nagai, Ryosuke Sawamura and Keisuke Asai
403.[] Characteristics of Thermal Anemometers at Low-Pressure Condition in a Mars Wind Tunnel.[49th AIAA Aerospace Science Meeting and Exhibit,(2010)]D. Numata, M. Anyoji, Y. Sugino, H. NAGAI and K. ASAI
404.[] Aerodynamic Measurements in the Mars Wind Tunnel at Tohoku University.[49th AIAA Aerospace Science Meeting and Exhibit,(2010)]M. Anyoji, K. Nose, S. Ida, D. Numata, H. Nagai and K. Asai
405.[] Unsteady PSP Technique for Measuring Naturally-Disturbed Periodic Phenomena.[48th AIAA Aerospace Science Meeting and Exhibit,(2010)]YORITA, D., NAGAI, H., ASAI, K., NARUMI, T.
406.[] Characteristics of the Mars Wind Tunnel at Tohoku University in CO2 Operation Mode.[48th AIAA Aerospace Science Meeting and Exhibit,(2010)]ANYOJI, M., IDA, S., NOSE, K., NUMATA, D., NAGAI, H., ASAI, K.
407.[] Simulation of the trajectory of a punted rugby ball taking into account the asymmetrical pressure distribution caused by the seams.[Journal of Visualization,1,(2010),449-456]Kazuya Seo, Osamu Kobayashi, Masahide Murakami, Daisuke Yorita, Hiroki Nagai, Keisuke Asai
408.[] Multi-objective exploration of the launch condition for a fluctuating punted kick in rugby on the basis of PSP measurement.[Procedia Engineering,2,(2010),2499-2504]Kazuya Seo, Daisuke Yorita, Koji Shimoyama, Hiroki Nagai and Keisuke Asai
10.1016/j.proeng.2010.04.022
409.[] 小型ループヒートパイプのリザーバ制御による動作特性の向上.[日本航空宇宙学会誌,(2010)]福吉芙由子,長野方星,小川博之,永井大樹
410.[] ループヒートパイプの熱特性における作動流体封入量の影響.[Thermal Science and Engineering,18(1),(2010),9-15]小野川英,長野方星,福吉芙由子,小川博之,永井大樹
411.[] Effect of Amount of Fluid Charge in Thermal Performance of Loop Heat Pipe.[Heat Transfer- Asian Research,(2010)]Hosei Nagano, Ei Onogawa, Fuyuko Fukuyoshi, Hiroyuki Ogawa, and Hiroki Nagai
412.[] Simulation of the trajectory of a punted rugby ball taking into account the asymmetrical pressure distribution caused by the seams.[Journal of Visualization,13(2),(2010),97-105]Kazuya Seo, Osamu Kobayashi, Masahide Murakami, Daisuke Yorita, Hiroki Nagai and Keisuke Asai
10.1007/s12650-009-0019-0
413.[] Unsteady PSP technique for measuring naturally-disturbed periodic phenomena.[48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, (2010)]D. Yorita, H. Nagai, K. Asai, T. Narumi
http://www.scopus.com/inward/record.url?eid=78649853229&partnerID=40
414.[] フォスファーとセラミック化合物による高温測定用感温塗料の試作と評価 (第38回可視化情報シンポジウム講演論文集) -- (オーガナイズドセッション 分子によるセンシングとイメージング(1)).[可視化情報学会誌,30(0), (2010), 173-176]澤村 亮輔, 永井 大樹, 沼田 大樹
415.[] 1501 カルマン渦が誘起する非定常圧力場の感圧塗料計測(OS15-1 先端的熱流体計測法,オーガナイズドセッション).[流体工学部門講演会講演論文集,2010(0), (2010), 435-436]依田 大輔, 沼田 大樹, 永井 大樹, 浅井 圭介
10.1299/jsmefed.2010.435
416.[] W0503-(2) 機能性分子センサーを用いた極限環境下における熱流体計測法(【W0503】EFDワークショップ『PSPによる表面情報の可視化計測』,ワークショップ).[年次大会講演資料集,2010(0), (2010), 159-160]永井 大樹
10.1299/jsmemecjsm.2010.9.0_159
417.[] 小型ループヒートパイプのリザーバ制御による動作特性の向上.[航空宇宙技術,9(9), (2010), 49-55]福吉 芙由子, 長野 方星, 小川 博之, 永井 大樹
10.2322/astj.9.49
418.[] カルマン渦が誘起する非定常圧力場の感圧塗料計測.[日本機械学会流体工学部門講演会講演論文集(CD-ROM),88th, (2010), ROMBUNNO.1501-]依田大輔, 沼田大樹, 永井大樹, 浅井圭介
419.[] 火星大気風洞の動作特性評価―現状と計画―.[日本航空宇宙学会年会講演会講演集(CD-ROM),41st, (2010), ROMBUNNO.C07-]安養寺正之, 野瀬慶, 沼田大樹, 永井大樹, 浅井圭介
420.[] 低圧環境下における熱線流速計の感度特性.[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),42nd-2010, (2010), ROMBUNNO.2C13-]沼田大樹, 杉野泰啓, 安養寺正之, 永井大樹, 浅井圭介
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