著書論文等- 永井 大樹 -
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件数:683件
[2011]
341.[] Evaluation of Aerodynamic Characteristics of a Triangular Airfoil at Low Reynolds Number and High-Subsonic Mach Number.[Proceedings of the Eighth International Conference on Flow Dynamics,(2011)]Suwa, T., Nose, K., Numata, D., Nagai, H., and Asai K.
342.[] Aerial Deployment Test of a Small UAV for Mars Exploration Flight.[Proceedings of the Eighth International Conference on Flow Dynamics,(2011),340-341]Fujita, K., Nagai, H., Asai, K. and Tokutake, H.
343.[] Conceptual Examination of a Small UAV for Mars Exploration Flight.[Proceedings of the Eighth International Conference on Flow Dynamics,(2011),448-449]Fujita, K., Nagai, H. and Asai, K,
344.[] Unsteady Aerodynamic Experiment of NACA0012 Airfoil at Low Reynolds Number.[Proceedings of the Eighth International Conference on Flow Dynamics,(2011)]Nose, K., Sakai, N., Numata, D., Nagai, H., Asai, K., Ikeda, T. and Atobe, T.
345.[] High-accuracy Calculation for Aerodynamic Heating Using Temperature-Sensitive Paint.[Proceedings of the Eighth International Conference on Flow Dynamics,(2011),552-553]Nishigata, K., Sawamura, R., Nagai, H., and Asai, K.
346.[] Development of Temperature-Sensitive Paint for High-Temperature Measurement.[Proceedings of the Eighth International Conference on Flow Dynamics,(2011),558-559]Sawamura, R., Nishigata, K., Nagai, H., and Asai, K.
347.[] Heat Transfer Characteristics of Oscillating Heat Pipe by Difference of Surface Characteristic.[Proceedings of the Eighth International Conference on Flow Dynamics,(2011),556-557]Kanayama, T., Daimaru, T., Nagai, H., Ogawa, H.
348.[] Development of an experimental small loop heat pipe with polytetrafluoroethylene wicks.[Journal of Thermophysics and Heat Transfer,25,(2011),547-552]Hosei Nagano, Fuyuko Fukuyoshi, Hiroyuki Ogawa, Hiroki Nagai
10.2514/1.T3614
http://www.scopus.com/inward/record.url?eid=80054077357&partnerID=40
349.[] バルク超伝導体を利用した小型磁場発生装置の開発.[東北大学金属材料研究所強磁場超伝導材料研究センター年次報告,2010, (2011), 177-180]安部隆士, 山田和彦, 新倉脩平, 服部盛正, 永井大樹, 淡路智
350.[] ループヒートパイプの作動特性に対する重力加速度の影響.[日本混相流学会年会講演会講演論文集,2011, (2011), 126-127]永井大樹, 玉村大道, 真籠耕平, 長野方星, 小川博之
351.[] "SUPERSONIC WIND TUNNEL EXPERIMENT ON AERODYNAMIC CHARACTERISTICS AND WINGLETS EFFECTS OF THE TAPERED SUPERSONIC BIPLANE.[AJK2011-15015, Proceedings of ASME-JSME-KSME Joint Fluids Engineering Conference 2011, AJK2011-FED,(2011)]Fujisono, T., Yamashita, H., Toyoda, A., Nagai, H., Asai, K., Matsuno, T., Kawazoe, H., Jeong, S. and Obayashi, S.
352.[] 感圧塗料を用いた非定常空気力計測.[可視化情報学会誌,31(Suppl.1), (2011), 277-280]依田大輔, 山崎真一, 沼田大樹, 永井大樹, 浅井圭介
353.[] 極低温キャビテーション試験に適用可能な感温塗料の開発と評価.[可視化情報学会誌,31(Suppl.1), (2011), 273-276]藤井祥太, 新井山一樹, 永井大樹, 浅井圭介
354.[] 感温塗料による空力加熱計測手法の高精度化.[可視化情報学会誌,31(Suppl.1), (2011), 269-272]西潟一樹, 澤村亮輔, 永井大樹, 浅井圭介
355.[] PSP Measurement of Pressure Distribution on a Cambered Airfoil for Mars Exploration Airplane.[Proceedings of the 11th Asian Symposium on Visualization,(2011)]Nose, K., Anyoji, M., Numata, D., Nagai, H. and Asai, K.
356.[] Evaluation of Transfer Function of Pressure-Sensitive Paint for Unsteady Flow Measurement.[Proceedings of the 11th Asian Symposium on Visualization,(2011)]T. Sugimoto, D. Yorita, D. Numata, H. Nagai, K. Asai
357.[] Evaluation of Temperature-Sensitive Paint using Thermographic Phosphor by Hypersonic Aerodynamic Heating.[Proceedings of the 11th Asian Symposium on Visualization,(2011)]Sawamura, R., Nishigata, K., Nagai, H., Asai, K.
358.[] Surface pressure and flow field behind an oscillating fence submerged in turbulent boundary layer.[Experiments in Fluids,50(3),(2011),701-714]Manjinder Singh, Jonathan W. Naughton, Taro Yamashita, Hiroki Nagai, Keisuke Asai
10.1007/s00348-010-0977-y
http://gateway.isiknowledge.com/gateway/Gateway.cgi?&GWVersion=2&SrcAuth=TohokuUniv&SrcApp=TohokuUniv&DestLinkType=FullRecord&KeyUT=WOS:000287584300016&DestApp=WOS http://www.scopus.com/inward/record.url?eid=79954573462&partnerID=40
359.[] Development of a small He II cryostat with optical windows for a microgravity experiment.[CRYOGENICS,51(1), (2011), 74-78]N. Kimura, S. Takada, S. Gotoh, H. Kawamata, M. Iida, M. Murakami, H. Nagai, M. Mamiya
10.1016/j.cryogenics.2010.10.008
http://gateway.isiknowledge.com/gateway/Gateway.cgi?&GWVersion=2&SrcAuth=TohokuUniv&SrcApp=TohokuUniv&DestLinkType=FullRecord&KeyUT=WOS:000286848300012&DestApp=WOS
360.[] Surface Pressure and Flow Field Behind an Oscillating Fence Submerged in a Turbulent Boundary Layer, Experiments in Fluids.[Experiments in Fluids,(2011),701-714]Singh, M., Naughton, J.W., Yamashita, T., Nagai, H., Asai, K.
0.1007/s00348-010-0977-y
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