著書論文等- 永井 大樹 -
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件数:694件
[2009]
481.[] 月面長期滞在に向けた高性能ループヒートパイプの研究.[日本航空宇宙学会北部支部講演会ならびに再使用型宇宙推進系シンポジウム講演論文集,2009-10th, (2009), 239-242]長野方星, 福吉芙由子, 小川博之, 永井大樹
482.[] 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.[日本伝熱シンポジウム講演論文集(CD-ROM),46th, (2009), ROMBUNNO.G-312-]小野川英, 長野方星, 福吉芙由子, 小川博之, 永井大樹
483.[] 低圧下におけるDBDプラズマアクチュエータの作動特性.[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,41st-2009, (2009), 285-288]高垣雅彦, 永井大樹, 浅井圭介
484.[] トンネル内を走行する高速列車に生じる振動現象.[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,41st-2009, (2009), 107-110]小寺健幸, 永井大樹, 浅井圭介, 寺島修
485.[] 熱電変換モジュールを用いたループヒートパイプ動作特性のアクティブ制御.[日本伝熱シンポジウム講演論文集(CD-ROM),46th, (2009), ROMBUNNO.G-321-]福吉芙由子, 長野方星, 小川博之, 永井大樹
486.[] 小型ループヒートパイプの重力効果による熱輸送特性評価.[日本伝熱シンポジウム講演論文集(CD-ROM),46th, (2009), ROMBUNNO.G-333-]永井大樹, 長野方星, 福吉芙由子, 小川博之
487.[] 火星大気風洞の測定部気流特性について(第一報).[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,41st-2009, (2009), 211-214]安養寺正之, 伊田真悟, 永井大樹, 浅井圭介
488.[] 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]
489.[] 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
490.[] 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.
491.[] 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.
492.[] 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.
493.[] An experimental study of plasma actuator performance in martian atmospher.[5th International Conference on Flow Dynamics,(2008)]TAKAGAKI, M., NAGAI, H. and ASAI, K.
494.[] 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.
495.[] 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.
496.[] Flow-induced Vibration of a High-speed Train Running in a Tunnel.[Proceedings of KSAS-JSASS Joint International Symposium on Aerospace Engineering, (2008), 267-272]Takeyuki KODERA, Hiroki NAGAI, Keisuke-ASAI, Osamu Terashima
497.[] 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
498.[] Luminescent Differential-Pressure Sensor Based on Gas Transfer through Porous Membrane.[13th International Symposium on Flow Visualization,(2008)]YORITA, D., NAGAI, H., ASAI, K..
499.[] 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.
500.[] 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.
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