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:705件
[2010]
401.[] 低レイノルズ数領域における翼面圧力分布の感圧塗料計測.[可視化情報学会誌,30(Suppl.1), (2010), 201-206]野瀬慶, 小野直志, 安養寺正之, 沼田大樹, 永井大樹, 浅井圭介
402.[] 寿命法による圧力・温度同時計測光ファイバーセンサーの開発.[可視化情報学会誌,30(Suppl.1), (2010), 195-200]須貝直之, 依田大輔, 沼田大樹, 永井大樹, 浅井圭介
403.[] 高応答型感圧塗料の周波数特性.[可視化情報学会誌,30(Suppl.1), (2010), 177-180]杉本珠生, 依田大輔, 沼田大樹, 永井大樹, 浅井圭介
404.[] Development of Aerodynamic Heating Measurement Technique Using Temperaturesensitive Paint in Hypersonic Flow.[The 14th International Symposium on Flow Visualization,(2010)]Ha, S., Sawamura, R., Nagai, H., Asai, K.
405.[] Measuring Unsteady Low-Speed Flow Phenomena by Using a Time-Series Analysis of Pressure-Sensitive Paint Images.[The 14th International Symposium on Flow Visualization,(2010)]Yorita, D., Numata, D., Nagai, H., Asai, K.
406.[] Visualization of a Three-Dimensional Shock-Wave Structures in a Supersonic Busemann Biplane by Sharp Focusing Schlieren System and PSP Measurement.[The 14th International Symposium on Flow Visualization,(2010)]Hagiwara, M., Nagai, H., Numata, D., Asai, K.
407.[] Imaging Measurement of Skin Friction Field around Bluff Body Using Luminescent Oil Film Technique.[The 14th International Symposium on Flow Visualization,(2010)]Kakuta, T., Koyama, A., Yorita, D., Numata, D., Nagai, H., Asai, K., Woodiga, S.A., Liu, T.
408.[] Development of Pressure-Sensitive Paint Technique for Surface Pressure Measurement in a Mars Wind Tunnel.[The 14th International Symposium on Flow Visualization,(2010)]Ono, T., Anyoji, M., Ida, S., Nose, K., Numata, D., Nagai, H., Asai, K.
409.[] 感温塗料を用いた極超音速流れにおける圧縮コーナー模型表面の温度分布計測.[衝撃波シンポジウム講演論文集,2009, (2010), 53-56]永井大樹, HA Seungwoh, 澤村亮輔, 浅井圭介
410.[] 断層シュリーレン法と感圧塗料の複合計測による超音速複葉翼の3次元内部構造の可視化計測.[衝撃波シンポジウム講演論文集,2009, (2010), 29-32]萩原真澄, 永井大樹, 沼田大樹, 浅井圭介
411.[] Oxygen-sensing properties of 5, 10, 15, 20-tetraphenylporphinato platinum(II) and palladium(II) covalently bound on poly(isobutyl-co-2,2,2-trifluoroethyl methacrylate).[Journal of Polymer Science, Part A: Polymer Chemistry,48(3),(2010),663-670]Makoto Obata, Noriko Matsuura, Kazunori Mitsuo, Hiroki Nagai, Keisuke Asai, Masafumi Harada, Shiho Hirohara, Masao Tanihara, Shigenobu Yano
10.1002/pola.23818
http://gateway.isiknowledge.com/gateway/Gateway.cgi?&GWVersion=2&SrcAuth=TohokuUniv&SrcApp=TohokuUniv&DestLinkType=FullRecord&KeyUT=WOS:000274254600018&DestApp=WOS http://www.scopus.com/inward/record.url?eid=75749150185&partnerID=40
412.[] 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.
413.[] 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
414.[] 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
415.[] 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
416.[] 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.
417.[] 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.
418.[] 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
419.[] 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
420.[] 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
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] [36] [next]
戻るこのページのトップへ
copyright(c)2005 Tohoku University