著書論文等- 永井 大樹 -
表示方法: 表示形式: 表示順:
[]:著書 []:論文 []:総説・解説記事
件数:683件
[2009]
481.[] Visualization study of film boiling in saturated He II under low gravity environment.[Proc. of ICEC 22, (2009), 377-382]N. Kimura, S. Takada, S. Gotoh, H. Kawamata, M. Iida, M. Murakami, H. Nakai, H. Nagai, M. Mamiya
[2008]
482.[] 高速車両に作用する流体力評価手法の検討.[日本機械学会交通・物流部門大会講演論文集,17th, (2008), 61-64]寺島修, 阿部行伸, 小寺健幸, 永井大樹, 浅井圭介
483.[] Experimental study on three-dimensional shock interference flow of a supersonic Busemann Biplane.[KSAS/JSASS Joint Int'l Symposium on Aerospace Engineering 2008,(2008)]OYAMA, S., NAGAI, H., ASAI, K.
484.[] Flow-induced vibration of a High-speed Train Running in a Tunnel.[KSAS/JSASS Joint Int'l Symposium on Aerospace Engineering 2008,(2008)]KODERA, T., NAGAI, H., ASAI, K., TERASHIMA, O.
485.[] Visualization of the heat flux distribution on a blunt-nosed body with an aerospike in hypersonic flow.[KSAS/JSASS Joint Int'l Symposium on Aerospace Engineering 2008,(2008)]HA, S. NAGAI, H., ASAI, K., NAKAKITA, K. and TSUBOI, N.
486.[] An experimental study of plasma actuator performance in martian atmospher.[5th International Conference on Flow Dynamics,(2008)]TAKAGAKI, M., NAGAI, H. and ASAI, K.
487.[] Design and construction of Mars Wind Tunnel for simulating atmospheric flight on Mars.[5th International Conference on Flow Dynamics,(2008)]ANYOJI, M., NAGAI, H. and ASAI, K.
488.[] PSP measurement of the leeward-side pressure distribution of a simplified car model in yaw.[5th International Conference on Flow Dynamics,(2008)]YORITA, D., NAGAI, H. and ASAI, K.
489.[] 小型ループヒートパイプの熱流動解析モデルの構築と実験的検証.[日本混相流学会年会講演会講演論文集,2008, (2008), 132-133]長野方星, 福吉芙由子, 小川博之, 永井大樹
490.[] Luminescent Differential-Pressure Sensor Based on Gas Transfer through Porous Membrane.[13th International Symposium on Flow Visualization,(2008)]YORITA, D., NAGAI, H., ASAI, K..
491.[] Pressure-Sensitive Paint Measurement of Unsteady Pressure Field behind an Oscillating Fence Actuator.[13th International Symposium on Flow Visualization,(2008)]YAMASHITA, T., NAGAI, H., ASAI, K., SINGH, M. AND NAUGHTON, J. W.
492.[] Visualization of Interacting Flow Field between Busemann's Biplane in Supersonic Flow.[13th International Symposium on Flow Visualization,(2008)]KURATANI, N., NAGAI, H., ASAI, K., OGAWA, T., OBAYASHI, S.
493.[] Experimental Study on Interference Flow of a Supersonic Busemann Biplane using Pressure-Sensitive Paint Technique.[International Council of the Aeronautical Sciences 2008,(2008)]NAGAI, H., OYAMA, S., OGAWA, T., KURATANI, N., ASAI, K.
494.[] 偏揺角のついた単純自動車模型の風下側圧力分布のPSP計測.[可視化情報学会誌,28(Suppl.1), (2008), 97-100]依田大輔, 永井大樹, 浅井圭介, 田中真悟, 石田圭太郎
10.3154/jvs.28.97
495.[] Evaluation of Plasma Actuator Performance in Martian Atmosphere for Applications to Mars Airplane.[38th Fluid Dynamics Conference,(2008)]TAKAGAKI, M., ISONO, S., NAGAI, H., ASAI, K.
496.[] Surface Pressure and Flow Field Behind an Oscillating Fence Submerged in Turbulent Boundary Layer.[26th AIAA Aerodynamic Measurement Technology and Ground Testing Conference,(2008)]SINGH, M., NAUGHTON, J. W., YAMASHITA, T., NAGAI, H. and ASAI, K.
497.[] 極超音速流中のエアロスパイク模型に流入する熱流束分布の可視化.[衝撃波シンポジウム講演論文集,2007, (2008), 349-352]HA Seungwon, 三浦悠佑, 永井大樹, 浅井圭介, 中北和之
498.[] 感温塗料を用いた空力加熱計測手法の東大柏極超音速風洞への適用.[衝撃波シンポジウム講演論文集,2007, (2008), 357-360]永井大樹, HA SeungWon, 三浦悠佑, 浅井圭介
499.[] 超音速複葉翼の衝撃波干渉流れに関する可視化研究.[衝撃波シンポジウム講演論文集,2007, (2008), 219-220]大山創史, 永井大樹, 倉谷尚志, 小川俊広, 浅井圭介
500.[] 超音速複葉翼の干渉流れに関する実験的研究.[宇宙航空研究開発機構特別資料 JAXA-SP-,(07-016), (2008), 22-27]永井大樹, 齋藤賢一, 小川俊広, 浅井圭介
Page: [prev] [1] [2] [3] [4] [5] [6] [7] [8] [9] [10] [11] [12] [13] [14] [15] [16] [17] [18] [19] [20] [21] [22] [23] [24] [25] [26] [27] [28] [29] [30] [31] [32] [33] [34] [35] [next]
戻るこのページのトップへ
copyright(c)2005 Tohoku University