論文- 永井 大樹 -
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件数:232件
[2010]
141.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
142.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
143.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.
144.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.
145.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
146.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
147.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
148.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
149.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
150.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
[2009]
151.Evaluation of Supersonic Ejector Driving Performance under Low Pressure.[6th International Conference on Flow Dynamics,(2009)]ANYOJI, M., NUMATA, D., NAGAI, H., ASAI, K.
152.Unsteady Pressure Distribution Measurement on a Square Cylinder using Pressure-Sensitive Paint.[6th International Conference on Flow Dynamics,(2009)]YORITA, D., NARUMI, T., NAGAI, H., ASAI, K.
153.Skin-Friction Measurement of Flow around Bluff Body Using Luminescent Oil-Film Technique.[6th International Conference on Flow Dynamics,(2009)]KAKUTA, T., KOYAMA, A., YORITA, D., NUMATA, D., NAGAI, H., ASAI, K.
154.Analysis of Shock-wave Structures in a Supersonic Busemann Biplane by Sharp Focusing Schlieren System.[6th International Conference on Flow Dynamics,(2009)]HAGIWARA, M., NAGAI, H., NUMATA, D., ASAI, K.
155.Application of Temperature-Sensitive Paint to Heat Flux Measurement in High Temperature Gas Flow.[6th International Conference on Flow Dynamics,(2009)]HA S., SAWAMURA, R.,SAKAMOTO, H., NAGAI, H., NUMATA, D., ASAI, K.
156.Optical Fiber Sensor Capable of Measuring Pressure and Temperature from Luminescent Lifetime.[6th International Conference on Flow Dynamics,(2009)]Sugai, N., Yorita, D., Numata, D., Nagai, H., Asai, K.
157.Three dimensional effect of a supersonic busemann biplane on start process.[27th International Symposium on Space Technology and Science,(2009)]NAGAI, H., OYAMA, S., ASAI, K., FUJISONO, T., OBAYASHI, S.
158.Experimental Study on the Thermal Performance of a Miniature Loop Heat Pipe with Different Orientations.[27th International Symposium on Space Technology and Science,(2009)]NAGAI, H., NAGANO, H., FUKUYOSHI, F., OGAWA, H.
159.Surface heat flux visualization on a blunt-nosed body with an aerospike in hypersonic flow using Temperature-Sensitive Paint.[27th International Symposium on Space Technology and Science,(2009)]NAGAI, H., HA, S., ASAI, K., TSUBOI, N., NAKAKITA, K.
160.Development of Low Density Wind Tunnel to Simulate Atmospheric Flight on Mars.[47th AIAA Aerospace Sciences Meeting,(2009)]ANYOJI, M., NAGAI, H., ASAI, K
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